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VA-Vol-37-No-11-Nov-2009

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Page 1: VA-Vol-37-No-11-Nov-2009

GEOFF ROBISON PRESIDEN T VINTAGE AIRCRAFT ASSOCIATION

Authority and potentials

Winter is now on the hoshyrizon here at home With the holidays just around the corner it wont be long before

Old Man Winter will be barking at us yet again Oh well my attitude has always been that the sooner it gets here the sooner its over I clearly remember just a few months ago reflecting about how long this past winter seemed to hang around here in Indiana It was a long and brutal one that I sure hope we dont see repeated

As I am writing this column I just returned from Oshkosh A bunch of our Vintage Aircraft Association (VAA) volunteers always get together in early October to winterize our campers that we use throughout the year when we attend the work parties and various other EAA events Its always a fun and laid-back weekend lacking the routine hustle and busshytle of preparing for EAA AirVenture Oshkosh Although we didnt have the best of weather this past weekend we sure made up for it in enthusiasm and a great deal of camaraderie Many thanks to all in attendance especially Bob Lumley and Georgia Schneider for preparing a great meal for us all on Saturday evening at the Aeroplane Factory on the EAA grounds

September was a very busy month for us here at the VAA Chapter 37 hangar It all started early in the month during the Labor Day weekshyend when we hosted New Standard barnstormer rides during the annual Auburn-Cord-Duesenberg Auto Festishy

val held every Labor Day weekend in Auburn Indiana If you havent had the opportunity to ride in a New Stanshydard you really need to experience this aircraft The crew of the New Standard is a bunch of crazy wing nuts so we had a really good time hosting them for this event Many thanks to Scooter and his crazy cast

The world of sport aviation

continues to face unprecedented

challenges t~ our right to fly

of aviators for a fun-filled weekend Our chapter also hosted the 2009

Stinson fly-in at Auburn in midshyOctober This was also a fun weekshyend with good weather and exshycellent attendance We topped off the month by hosting the EAA B-17 tour at Auburn Although the weather was a bit challenging we again enjoyed hosting the aircraft as well as the crew A good number of our local B-17 vets again showed up to share their experiences with hunshydreds of local visitors to the tour Thanks for coming guys We really enjoyed our time with you

Mix that all in with a couple of Young Eagles events and you can

see why I use the term busy Many thanks also go out to all of the local chapter volunteers who supported us in hosting all of these events We simply couldnt do it without you

The world of sport aviation conshytinues to face unprecedented chalshylenges to our right to fly It seems to me as though nearly every layer of government regulators seems to think that they arent doing th eir job unless they periodically fire a shot across our bow to make sure we havent forgotten about their aushythority But recently there was a bill introduced in the House of Represhysentatives that will potentially limit their authority to arbitrarily regulate those of us who are engaged in this pleasure we call aviation

On September 30 a good number of genera-aviation-minded representashytives introduced HR 3678 that would rein in the Department of Homeland Securitys (DHS) absolute power to isshysue security directives that severely impact aviation It seems as though the DHS has ruffled some feath ers inside the beltway with its incessant practices of issuing what are referred to as safety bulletins A number of which have included unwarranted impact on our access to free skies If this bill passes the House it would effectively limit DHS in its ability to arbitrarily pass security directives unshyless they prove to be in response to an imminent threat and then only for a maximum of 180 days If such a direcshytive needs to be in place for a period longer than 180 days the DHS would

continlled on page 39

ov B VOL 37 No 11 2009

CONTENTS I F e Straight amp Level

Authority and potentials by Geoff Robison

2 News

4 Rotary Dreams-The Restoration of a Pitcairn PA-I8 Autogiro

The Reserv_e Grand Champion Antique of EAA AirVenture Oshkosh 2009 by HG Frautschy with Nick Hurm

16 Miss Champion Pitcairn-Cierva Autogiro PCA-2 by Carl Gunther and Gene Chase

24 The Vintage Mechanic Materials amp Processes Part 2 by Robert G Lock

28 Light Plane Heritage The Mummert Cootie by Jack McRae

32 The Vintage Instructor All available info by Doug Stewart

34 Mystery Plane by HG Frautschy

39 Classified Ads

COVERS FRONT COVER This issue of Vintage Airplane is dedicated to vintage rotorcraft and this beautiful example is the 1931 Pitcairn PA-18 Autogiro restored by Jack Tiffany and the crew at Leading Edge Aircraft in Ohio Restored over a 9-year period it is the only Pitshycairn Autogiro currently flying Read more about it starting on page 4 EAA photo by HG Frautschy EAA Cessna 210 photo plane ftown by Janet Davidson

BACK COVER Now a part of the permanent collection of the EAA AirVenture Museum in Oshkosh this is Steve Pitcairn s restored Pitcairn PCA-2 on its final flight on a beautiful fall afternoon in 2005 before being donated to EAA Those who were present were treated

to a glorious flight display as Steve said goodbye to the oldest ftying rotorcraft then in America restored by George Townson and maintained by the Posey Brothers (who helped move Miss Champion to Oshkosh) Read more about it starting on page 16 EAA photo by HG Frautschy

1921 wMMfJlI CQQ]]pound

LAWRANCE ENGINE

j1j

STAFF EAA Publisher Tom Poberezny Director of EAA Publications Mary Jones Executive DirectorEditor HG Frautschy ProductionSpecial Project Kathleen Witman Photography Jim Koepnick

Bonnie Kratz Advertising Coordina tor Sue Anderson Classified Ad Coordinator Lesley Poberezny Copy Editor Colleen Wa lsh Director of Advertising Katrina Bradshaw

Display Advertisi ng Representatives Specialized Publications Co US Eastern Time Zone-Northeast Ken Ross 609-822-3750 Fax 609-957-5650 kr4 Ocomcastnet

US Eastern Time Zone-Southeast Chester Baumgartner 727-532-4640 Fax 727-532-4630 cbaum111mindspringcom

US Central Time Zone Gary Worden and Todd Reese 800-444-9932 Fax 816-74 1-6458 garywordenspc-magcom toddSpc-magcom

US Mountain and Pacific Time Zones John Gibson 916-784-9593 Fax 510-217-3796 iohngibsonspc-magcoln

Europe Willi Tacke Phone +49(0)1716980871 Fax +49(0)8841 496012 willilying-pagescom

VINTAGE AIRPLANE

Sully and Skiles New Young Eagles Co-Chairs

Sully Sullenberger (left) and Jeff Skiles co-chairs of the EAA Young Eagles program

EAA members expressed surprise and excitement when it was announced September 29 that US Airways Flight 1549 pilots Chesley Sully Sullenberger and Jeff Skiles would be the new co-chairs of EANs Young Eagles program

Many people have contacted me and said what a great choice it was unexshypected but what a great choice for the next step to lead the Young Eagles proshygram said EAA PresidentChairman Tom Poberezny You can read more about the new co-chairmen on page 81 of fAA Sport Aviation

Since vintage aircraft make up the majority of the lightplane general-aviation fleet it probably comes as no surprise to learn that the majority of the 15 million Young Eagles flown so far were flown in aircraft built priorto 1971 and one of the new Young Eagles chairmen expects that trend to continue for him in a very personal way you can read an interview with Jeff Skiles and see a slide show of his newWaco YOC in issue No 3 of Vintage Aircraft Online the VANs newest member benefit You can access it online at www EAAorg vintageaircraft

EAA Responds Immediately still trying to fix their broken busishyto Anti-GA Airport Stories ness model by inflaming the public Inaccurateclaims that small ai rportsreceive with one-sided media stories said disproportionate amount of federal money Tom Poberezny EAA chairmanpresishy

When two national news outlets dent For several years the airlines recently produced stories critical of have tried to shift the burden of supshyfunding for general-aviation (GA) porting our nations airport infrashyairports EAA and other aviation orshy structure by tossing it on the back of ganizations promptly stood up and general aviation It was wrong before set things straight USA Today and and it still is NBC ran stories on September 17 What the news ou tlets failed that claimed smaller airports receive to report is that aviation fuel taxes a disproportionately large amount of paid by GA annually exceed grants federal funding to upgrade those fashy distributed for all airport improveshycilities at the expense of the nations ments yet those funds are perennishycommercial hubs ally raided to ease the FAAs general

This is very upsetting but not unshy budget shortfall Hub airports also reshyexpected-its obvious the airlines are ceive three times more federal funds

NOVEMBER 2009

than do GA airports and GA users pay five times more in fuel taxes than the airlines to support the air traffic control system the primary users of which are the airlines

EAA agrees with one item from the USA Today story-the nations small airports are underutilized Poshyberezny said If major hub airports are overcrowded but smaller airports are ready and eager to serve aviashytion why would it make any sense to wage war on small airports They are all essential parts of the nations transportation system

EAAer Keys Mexican ElT Rule Extension

Thanks to coordination efforts by EAA member Rick Gardner EAA 791548 of travel service provider Cashyribbean Sky Tours the Mexican govshyernment extended its emergency loshycator transmitter (ELT) rules through April 2010 for general-aviation airshycraft flying in Mexico The extension provides a procedure that will allow certain US pilots operating 1215 MHz ELTs to fly into Mexicothrough April 2 2010 After that date all general-aviation aircraft flying into Mexico must be equipped with an operable 406 MHz ELT

Gardner and his wife Pia ownshyers and operators of Cancun Mexshyico-based Caribbean Sky Tours are longtime AirVenture and Sun n Fun exhibitors and regularly conduct foshyrums on flying to Mexico Central America and the Caribbean Rick Gardner worked directly with the Dishyreccion General De Aeronautica Civil (DGAC the Mexican equivalent of the FAA) on the 406 MHz ELT regulashytion for the last two years

We have had a very good relashytionship with the DGAC for many years and have worked together on a number of different issues to facilishytate the arrival of visiting general avishyation aircraft into Mexico he said We are also on the executive counshy

2

cil of the Mexican Federation of Pishylots (FEMPPA) and are an authorized distributor for INEGI the Mexican charting office which allows us to stay abreast of Mexican aeronautical issues and products

TSA and DHS Merge Border Flight Crossing Procedures

Two Department of Homeland Seshycurity (DHS) agencies recently merged their border security programs to eliminate redundancy as well as the paperwork burden of international travelers The Transportation Secushyrity Administrations (TSA) Internashytional Waiver program will be folded into Customs and Border Protections (CBP) Advanced Passenger Informashytion System (APIS)

This will satisfy a commitment made at AirVenture 2009 by TSAs new general-aviation manager Brian Deshylauter and CBPs APIS program manshyager Eric Rodriguez to improve the border-crossing procedure for generalshyaviation pilots through collaboration The info merger will allow pilots to complete only the CBP electronic APIS paperwork to fly across US borders

EAA which has advocated for a less onerous system has prepared a guide on how to navigate the current reshyquirements until the new process is fishynalized That is available at wwwEAA orgnews20092009-0S-21_cbpasp

VAA Volunteer of the Year Awards

During the fall board meeting Jim Swol (right) was presented with acommemorashytive clock and a certificate commemorating his selection as the 2009 Art Morgan VAA Flightline Volunteer of the Year

Each year the Vintage Aircraft Association honors two of its own for their service to the VAA and its members during the annual convention As it is every year its tough to pick just one person for such an honor but this year was especially challenging as we had afantastic group

of volunteers step it up an extra notch during the months prior to this years amazing event and during the convention

The Art Morgan VAA Flightline Volunteer of the Year comes to us all the way from the state of Maine For years we have both marveled and worried at the willingness of the VAA flightline volunteers to keep going and do whatever was requested of them and Jim Swol epitomizes that volunteer work ethic- always on the spot doing what needs to be done year after year

The VAA Behind the Scenes Volunteer of the Year is actually a twosome this year The wayshybeyond-the-call -of-duty work spearheaded by these two volunteers made it possible for us to comshyplete the Vintage Hangar on time and under budget Thanks to the work by Archie James and Michael Blombach this years honorees for the award the 40-plus volunteers who helped finish out the projshyect were kept busy and focused so that we could all enjoy our new facilities when AirVenture started

Our sincere admiration and heartfelt thanks to Jim Swol Archie James and Michael Blombach for their hard work Congratulations gentlemen

EAA Share the Spirit Sweepstakes This new Aviat Husky could be yours

Its on The 2010 EAA Share the Spirit Sweepshystakes website is now live and with it your chance to flyaway in the grand prize-a brand new fully equipped Aviat Husky A-1 C To top things off (includshying the 50-gallon fuel tank over and over again) the grand prize comes with a full years worth of fuel credit from Chevron plus 50000 points in Chevrons FlyBuys rewards program Equipped with a Garmin GsOO and GNS 430 panel-mount avionics suite and a set ofWipaire C2200 hydrauliC wheel skis the grand prize Husky will take you places youve never been

But you have to enter and fortunately there are many ways to do so (Entry coupons are included in the November issue of Sport Aviation and will also be included in the 2010 January March and May issues of EAAs flagship magazine) Or you can enter anytime at wwwWinAPlanecom

Other top sweepstakes prizes include a Honda Big Red mUltipurpose utility vehicle REMOS Pilot Center sport pilot training certificate mens Hamilton Khaki X-Wind aviation watch Canon EOS SOD camera kit with lens and Bose Wave music system

VINTAGE AIRPLANE 3

so what would a former high school track star Army Speshycial Ops soldier and parashychute ace want for a vintage aircraft If youre a guy like

Jack Tiffany of Spring Valley Ohio youd go for the most unusual thing you could find-an Autogiro

There was only one problem for the energetic Tiffany a Vietnam vetshyeran now in his seventh decade he couldnt find one to restore Other neat projects came and went for his laid-back confederation of reshystorers that bill themselves as Leadshying Edge Aircraft (liOn the Trailing Edge of Technology is its motto) A Fairchild Kreider-Reisner 21 biplane a Fleet 16B a couple of Davis Dshy1Ws and a smattering of Wacos and other ancient but lovable aircraft passed through the hangar doors but an Autogiro proved elusive He searched for one for 28 years

Enter the third generation of aviashytion fanatics in the Tiffany sphere of influence Jacks father had been an Air Force crew chief and for Jack aviation was a major part of his life Later when he married Kate (an avowed aviation nut herself shes

NOVEMBER 2009

HG fRAUT SCHY

6

served as a volunteer judge at EAA AirVenture Oshkosh) he got a boshynus in the bargain Kates son Nick The young boy soon became as enshyamored as his stepfather with aviashytion and as a teenager Nick became quite the aviation sleuth digging up tidbits of handy aviation knowledge That tenacity would payoff in 1999 when he came to Jack with the reveshylation that there was an Autogiro out there that could be restored In fact there were two

It didnt take long for Jack and Nick to track down Al Letcher of Moshyjave California AI a longtime colshylector of vintage aircraft had bought the remains of a Pitcairn PA-18 from Ted Sowirka who had owned it for 43 years But how it came to be in his hands is a story that will warm the

heart of many a potential restorer who still has hopes of finding his own aeronautical Holy Grail

History The Pitcairn PA-18 Autogiro was

created by the company after the firm had created quite a name for itshyself with the PCA-2 Autogiro a large expensive craft that was bought by a few firms for its novel appearance which since it attracted a lot of atshytention made it a suitable platform for advertising But the PCA-2 with a 300-hp Wright Whirlwind on the nose and a 4S-foot rotor span was a big rotorcraft It could carry three with ease and its hulking presence on the ground made it hard to miss (Autogiro with a capital A is the spelling coined by the Cierva Auto-

Since it is a fixed-spindle system the rotor head is relatively simple The cables and the bungee cords attached to them act as limit stops when the rotor is rotating slowly or is stopped To the sides of the rotorshyattach hinges are the squarish rubshyber pads that in combination with the dampers installed farther out on each blade act to dampen and limit the leadlag movement of each rotor blade as it flies around the rotor disc To the left is the pre-rotator gearbox which engages with the helical spur gear bolted to the bottom of the roshytor head The pre-rotator is used to spin up the rotor blades to a stable rpm before the takeoff roll is started Having a spun-up rotor allows the rotor to be started and brought up to speed without the hazard of taxiing with a low-speed unstable rotor sysshytem and it significantly reduces the takeoff run

By necessity the rotor blades are quite flexible which require the trailing edge of each blade to be segmented This leather patch on the trailing edge covers one of the slip joints on the trailing edge

When running the short stacks on the 160-hp five-cylinder Kinner-R-55 give the Pitcairn a distinctive bark in flight

VINTAGE AIRPLANE 7

After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

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DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

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Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

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DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

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chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

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Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

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Page 2: VA-Vol-37-No-11-Nov-2009

ov B VOL 37 No 11 2009

CONTENTS I F e Straight amp Level

Authority and potentials by Geoff Robison

2 News

4 Rotary Dreams-The Restoration of a Pitcairn PA-I8 Autogiro

The Reserv_e Grand Champion Antique of EAA AirVenture Oshkosh 2009 by HG Frautschy with Nick Hurm

16 Miss Champion Pitcairn-Cierva Autogiro PCA-2 by Carl Gunther and Gene Chase

24 The Vintage Mechanic Materials amp Processes Part 2 by Robert G Lock

28 Light Plane Heritage The Mummert Cootie by Jack McRae

32 The Vintage Instructor All available info by Doug Stewart

34 Mystery Plane by HG Frautschy

39 Classified Ads

COVERS FRONT COVER This issue of Vintage Airplane is dedicated to vintage rotorcraft and this beautiful example is the 1931 Pitcairn PA-18 Autogiro restored by Jack Tiffany and the crew at Leading Edge Aircraft in Ohio Restored over a 9-year period it is the only Pitshycairn Autogiro currently flying Read more about it starting on page 4 EAA photo by HG Frautschy EAA Cessna 210 photo plane ftown by Janet Davidson

BACK COVER Now a part of the permanent collection of the EAA AirVenture Museum in Oshkosh this is Steve Pitcairn s restored Pitcairn PCA-2 on its final flight on a beautiful fall afternoon in 2005 before being donated to EAA Those who were present were treated

to a glorious flight display as Steve said goodbye to the oldest ftying rotorcraft then in America restored by George Townson and maintained by the Posey Brothers (who helped move Miss Champion to Oshkosh) Read more about it starting on page 16 EAA photo by HG Frautschy

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STAFF EAA Publisher Tom Poberezny Director of EAA Publications Mary Jones Executive DirectorEditor HG Frautschy ProductionSpecial Project Kathleen Witman Photography Jim Koepnick

Bonnie Kratz Advertising Coordina tor Sue Anderson Classified Ad Coordinator Lesley Poberezny Copy Editor Colleen Wa lsh Director of Advertising Katrina Bradshaw

Display Advertisi ng Representatives Specialized Publications Co US Eastern Time Zone-Northeast Ken Ross 609-822-3750 Fax 609-957-5650 kr4 Ocomcastnet

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US Central Time Zone Gary Worden and Todd Reese 800-444-9932 Fax 816-74 1-6458 garywordenspc-magcom toddSpc-magcom

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VINTAGE AIRPLANE

Sully and Skiles New Young Eagles Co-Chairs

Sully Sullenberger (left) and Jeff Skiles co-chairs of the EAA Young Eagles program

EAA members expressed surprise and excitement when it was announced September 29 that US Airways Flight 1549 pilots Chesley Sully Sullenberger and Jeff Skiles would be the new co-chairs of EANs Young Eagles program

Many people have contacted me and said what a great choice it was unexshypected but what a great choice for the next step to lead the Young Eagles proshygram said EAA PresidentChairman Tom Poberezny You can read more about the new co-chairmen on page 81 of fAA Sport Aviation

Since vintage aircraft make up the majority of the lightplane general-aviation fleet it probably comes as no surprise to learn that the majority of the 15 million Young Eagles flown so far were flown in aircraft built priorto 1971 and one of the new Young Eagles chairmen expects that trend to continue for him in a very personal way you can read an interview with Jeff Skiles and see a slide show of his newWaco YOC in issue No 3 of Vintage Aircraft Online the VANs newest member benefit You can access it online at www EAAorg vintageaircraft

EAA Responds Immediately still trying to fix their broken busishyto Anti-GA Airport Stories ness model by inflaming the public Inaccurateclaims that small ai rportsreceive with one-sided media stories said disproportionate amount of federal money Tom Poberezny EAA chairmanpresishy

When two national news outlets dent For several years the airlines recently produced stories critical of have tried to shift the burden of supshyfunding for general-aviation (GA) porting our nations airport infrashyairports EAA and other aviation orshy structure by tossing it on the back of ganizations promptly stood up and general aviation It was wrong before set things straight USA Today and and it still is NBC ran stories on September 17 What the news ou tlets failed that claimed smaller airports receive to report is that aviation fuel taxes a disproportionately large amount of paid by GA annually exceed grants federal funding to upgrade those fashy distributed for all airport improveshycilities at the expense of the nations ments yet those funds are perennishycommercial hubs ally raided to ease the FAAs general

This is very upsetting but not unshy budget shortfall Hub airports also reshyexpected-its obvious the airlines are ceive three times more federal funds

NOVEMBER 2009

than do GA airports and GA users pay five times more in fuel taxes than the airlines to support the air traffic control system the primary users of which are the airlines

EAA agrees with one item from the USA Today story-the nations small airports are underutilized Poshyberezny said If major hub airports are overcrowded but smaller airports are ready and eager to serve aviashytion why would it make any sense to wage war on small airports They are all essential parts of the nations transportation system

EAAer Keys Mexican ElT Rule Extension

Thanks to coordination efforts by EAA member Rick Gardner EAA 791548 of travel service provider Cashyribbean Sky Tours the Mexican govshyernment extended its emergency loshycator transmitter (ELT) rules through April 2010 for general-aviation airshycraft flying in Mexico The extension provides a procedure that will allow certain US pilots operating 1215 MHz ELTs to fly into Mexicothrough April 2 2010 After that date all general-aviation aircraft flying into Mexico must be equipped with an operable 406 MHz ELT

Gardner and his wife Pia ownshyers and operators of Cancun Mexshyico-based Caribbean Sky Tours are longtime AirVenture and Sun n Fun exhibitors and regularly conduct foshyrums on flying to Mexico Central America and the Caribbean Rick Gardner worked directly with the Dishyreccion General De Aeronautica Civil (DGAC the Mexican equivalent of the FAA) on the 406 MHz ELT regulashytion for the last two years

We have had a very good relashytionship with the DGAC for many years and have worked together on a number of different issues to facilishytate the arrival of visiting general avishyation aircraft into Mexico he said We are also on the executive counshy

2

cil of the Mexican Federation of Pishylots (FEMPPA) and are an authorized distributor for INEGI the Mexican charting office which allows us to stay abreast of Mexican aeronautical issues and products

TSA and DHS Merge Border Flight Crossing Procedures

Two Department of Homeland Seshycurity (DHS) agencies recently merged their border security programs to eliminate redundancy as well as the paperwork burden of international travelers The Transportation Secushyrity Administrations (TSA) Internashytional Waiver program will be folded into Customs and Border Protections (CBP) Advanced Passenger Informashytion System (APIS)

This will satisfy a commitment made at AirVenture 2009 by TSAs new general-aviation manager Brian Deshylauter and CBPs APIS program manshyager Eric Rodriguez to improve the border-crossing procedure for generalshyaviation pilots through collaboration The info merger will allow pilots to complete only the CBP electronic APIS paperwork to fly across US borders

EAA which has advocated for a less onerous system has prepared a guide on how to navigate the current reshyquirements until the new process is fishynalized That is available at wwwEAA orgnews20092009-0S-21_cbpasp

VAA Volunteer of the Year Awards

During the fall board meeting Jim Swol (right) was presented with acommemorashytive clock and a certificate commemorating his selection as the 2009 Art Morgan VAA Flightline Volunteer of the Year

Each year the Vintage Aircraft Association honors two of its own for their service to the VAA and its members during the annual convention As it is every year its tough to pick just one person for such an honor but this year was especially challenging as we had afantastic group

of volunteers step it up an extra notch during the months prior to this years amazing event and during the convention

The Art Morgan VAA Flightline Volunteer of the Year comes to us all the way from the state of Maine For years we have both marveled and worried at the willingness of the VAA flightline volunteers to keep going and do whatever was requested of them and Jim Swol epitomizes that volunteer work ethic- always on the spot doing what needs to be done year after year

The VAA Behind the Scenes Volunteer of the Year is actually a twosome this year The wayshybeyond-the-call -of-duty work spearheaded by these two volunteers made it possible for us to comshyplete the Vintage Hangar on time and under budget Thanks to the work by Archie James and Michael Blombach this years honorees for the award the 40-plus volunteers who helped finish out the projshyect were kept busy and focused so that we could all enjoy our new facilities when AirVenture started

Our sincere admiration and heartfelt thanks to Jim Swol Archie James and Michael Blombach for their hard work Congratulations gentlemen

EAA Share the Spirit Sweepstakes This new Aviat Husky could be yours

Its on The 2010 EAA Share the Spirit Sweepshystakes website is now live and with it your chance to flyaway in the grand prize-a brand new fully equipped Aviat Husky A-1 C To top things off (includshying the 50-gallon fuel tank over and over again) the grand prize comes with a full years worth of fuel credit from Chevron plus 50000 points in Chevrons FlyBuys rewards program Equipped with a Garmin GsOO and GNS 430 panel-mount avionics suite and a set ofWipaire C2200 hydrauliC wheel skis the grand prize Husky will take you places youve never been

But you have to enter and fortunately there are many ways to do so (Entry coupons are included in the November issue of Sport Aviation and will also be included in the 2010 January March and May issues of EAAs flagship magazine) Or you can enter anytime at wwwWinAPlanecom

Other top sweepstakes prizes include a Honda Big Red mUltipurpose utility vehicle REMOS Pilot Center sport pilot training certificate mens Hamilton Khaki X-Wind aviation watch Canon EOS SOD camera kit with lens and Bose Wave music system

VINTAGE AIRPLANE 3

so what would a former high school track star Army Speshycial Ops soldier and parashychute ace want for a vintage aircraft If youre a guy like

Jack Tiffany of Spring Valley Ohio youd go for the most unusual thing you could find-an Autogiro

There was only one problem for the energetic Tiffany a Vietnam vetshyeran now in his seventh decade he couldnt find one to restore Other neat projects came and went for his laid-back confederation of reshystorers that bill themselves as Leadshying Edge Aircraft (liOn the Trailing Edge of Technology is its motto) A Fairchild Kreider-Reisner 21 biplane a Fleet 16B a couple of Davis Dshy1Ws and a smattering of Wacos and other ancient but lovable aircraft passed through the hangar doors but an Autogiro proved elusive He searched for one for 28 years

Enter the third generation of aviashytion fanatics in the Tiffany sphere of influence Jacks father had been an Air Force crew chief and for Jack aviation was a major part of his life Later when he married Kate (an avowed aviation nut herself shes

NOVEMBER 2009

HG fRAUT SCHY

6

served as a volunteer judge at EAA AirVenture Oshkosh) he got a boshynus in the bargain Kates son Nick The young boy soon became as enshyamored as his stepfather with aviashytion and as a teenager Nick became quite the aviation sleuth digging up tidbits of handy aviation knowledge That tenacity would payoff in 1999 when he came to Jack with the reveshylation that there was an Autogiro out there that could be restored In fact there were two

It didnt take long for Jack and Nick to track down Al Letcher of Moshyjave California AI a longtime colshylector of vintage aircraft had bought the remains of a Pitcairn PA-18 from Ted Sowirka who had owned it for 43 years But how it came to be in his hands is a story that will warm the

heart of many a potential restorer who still has hopes of finding his own aeronautical Holy Grail

History The Pitcairn PA-18 Autogiro was

created by the company after the firm had created quite a name for itshyself with the PCA-2 Autogiro a large expensive craft that was bought by a few firms for its novel appearance which since it attracted a lot of atshytention made it a suitable platform for advertising But the PCA-2 with a 300-hp Wright Whirlwind on the nose and a 4S-foot rotor span was a big rotorcraft It could carry three with ease and its hulking presence on the ground made it hard to miss (Autogiro with a capital A is the spelling coined by the Cierva Auto-

Since it is a fixed-spindle system the rotor head is relatively simple The cables and the bungee cords attached to them act as limit stops when the rotor is rotating slowly or is stopped To the sides of the rotorshyattach hinges are the squarish rubshyber pads that in combination with the dampers installed farther out on each blade act to dampen and limit the leadlag movement of each rotor blade as it flies around the rotor disc To the left is the pre-rotator gearbox which engages with the helical spur gear bolted to the bottom of the roshytor head The pre-rotator is used to spin up the rotor blades to a stable rpm before the takeoff roll is started Having a spun-up rotor allows the rotor to be started and brought up to speed without the hazard of taxiing with a low-speed unstable rotor sysshytem and it significantly reduces the takeoff run

By necessity the rotor blades are quite flexible which require the trailing edge of each blade to be segmented This leather patch on the trailing edge covers one of the slip joints on the trailing edge

When running the short stacks on the 160-hp five-cylinder Kinner-R-55 give the Pitcairn a distinctive bark in flight

VINTAGE AIRPLANE 7

After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

II have been flying now for over 25 years I am a Certified

Flight Instructor and let me tell you - not only is the personal

hometown family feeling of dealing with AUA wonderful year

after year they find a way to insure my precious airplanes at a

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

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Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

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EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

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Page 3: VA-Vol-37-No-11-Nov-2009

Sully and Skiles New Young Eagles Co-Chairs

Sully Sullenberger (left) and Jeff Skiles co-chairs of the EAA Young Eagles program

EAA members expressed surprise and excitement when it was announced September 29 that US Airways Flight 1549 pilots Chesley Sully Sullenberger and Jeff Skiles would be the new co-chairs of EANs Young Eagles program

Many people have contacted me and said what a great choice it was unexshypected but what a great choice for the next step to lead the Young Eagles proshygram said EAA PresidentChairman Tom Poberezny You can read more about the new co-chairmen on page 81 of fAA Sport Aviation

Since vintage aircraft make up the majority of the lightplane general-aviation fleet it probably comes as no surprise to learn that the majority of the 15 million Young Eagles flown so far were flown in aircraft built priorto 1971 and one of the new Young Eagles chairmen expects that trend to continue for him in a very personal way you can read an interview with Jeff Skiles and see a slide show of his newWaco YOC in issue No 3 of Vintage Aircraft Online the VANs newest member benefit You can access it online at www EAAorg vintageaircraft

EAA Responds Immediately still trying to fix their broken busishyto Anti-GA Airport Stories ness model by inflaming the public Inaccurateclaims that small ai rportsreceive with one-sided media stories said disproportionate amount of federal money Tom Poberezny EAA chairmanpresishy

When two national news outlets dent For several years the airlines recently produced stories critical of have tried to shift the burden of supshyfunding for general-aviation (GA) porting our nations airport infrashyairports EAA and other aviation orshy structure by tossing it on the back of ganizations promptly stood up and general aviation It was wrong before set things straight USA Today and and it still is NBC ran stories on September 17 What the news ou tlets failed that claimed smaller airports receive to report is that aviation fuel taxes a disproportionately large amount of paid by GA annually exceed grants federal funding to upgrade those fashy distributed for all airport improveshycilities at the expense of the nations ments yet those funds are perennishycommercial hubs ally raided to ease the FAAs general

This is very upsetting but not unshy budget shortfall Hub airports also reshyexpected-its obvious the airlines are ceive three times more federal funds

NOVEMBER 2009

than do GA airports and GA users pay five times more in fuel taxes than the airlines to support the air traffic control system the primary users of which are the airlines

EAA agrees with one item from the USA Today story-the nations small airports are underutilized Poshyberezny said If major hub airports are overcrowded but smaller airports are ready and eager to serve aviashytion why would it make any sense to wage war on small airports They are all essential parts of the nations transportation system

EAAer Keys Mexican ElT Rule Extension

Thanks to coordination efforts by EAA member Rick Gardner EAA 791548 of travel service provider Cashyribbean Sky Tours the Mexican govshyernment extended its emergency loshycator transmitter (ELT) rules through April 2010 for general-aviation airshycraft flying in Mexico The extension provides a procedure that will allow certain US pilots operating 1215 MHz ELTs to fly into Mexicothrough April 2 2010 After that date all general-aviation aircraft flying into Mexico must be equipped with an operable 406 MHz ELT

Gardner and his wife Pia ownshyers and operators of Cancun Mexshyico-based Caribbean Sky Tours are longtime AirVenture and Sun n Fun exhibitors and regularly conduct foshyrums on flying to Mexico Central America and the Caribbean Rick Gardner worked directly with the Dishyreccion General De Aeronautica Civil (DGAC the Mexican equivalent of the FAA) on the 406 MHz ELT regulashytion for the last two years

We have had a very good relashytionship with the DGAC for many years and have worked together on a number of different issues to facilishytate the arrival of visiting general avishyation aircraft into Mexico he said We are also on the executive counshy

2

cil of the Mexican Federation of Pishylots (FEMPPA) and are an authorized distributor for INEGI the Mexican charting office which allows us to stay abreast of Mexican aeronautical issues and products

TSA and DHS Merge Border Flight Crossing Procedures

Two Department of Homeland Seshycurity (DHS) agencies recently merged their border security programs to eliminate redundancy as well as the paperwork burden of international travelers The Transportation Secushyrity Administrations (TSA) Internashytional Waiver program will be folded into Customs and Border Protections (CBP) Advanced Passenger Informashytion System (APIS)

This will satisfy a commitment made at AirVenture 2009 by TSAs new general-aviation manager Brian Deshylauter and CBPs APIS program manshyager Eric Rodriguez to improve the border-crossing procedure for generalshyaviation pilots through collaboration The info merger will allow pilots to complete only the CBP electronic APIS paperwork to fly across US borders

EAA which has advocated for a less onerous system has prepared a guide on how to navigate the current reshyquirements until the new process is fishynalized That is available at wwwEAA orgnews20092009-0S-21_cbpasp

VAA Volunteer of the Year Awards

During the fall board meeting Jim Swol (right) was presented with acommemorashytive clock and a certificate commemorating his selection as the 2009 Art Morgan VAA Flightline Volunteer of the Year

Each year the Vintage Aircraft Association honors two of its own for their service to the VAA and its members during the annual convention As it is every year its tough to pick just one person for such an honor but this year was especially challenging as we had afantastic group

of volunteers step it up an extra notch during the months prior to this years amazing event and during the convention

The Art Morgan VAA Flightline Volunteer of the Year comes to us all the way from the state of Maine For years we have both marveled and worried at the willingness of the VAA flightline volunteers to keep going and do whatever was requested of them and Jim Swol epitomizes that volunteer work ethic- always on the spot doing what needs to be done year after year

The VAA Behind the Scenes Volunteer of the Year is actually a twosome this year The wayshybeyond-the-call -of-duty work spearheaded by these two volunteers made it possible for us to comshyplete the Vintage Hangar on time and under budget Thanks to the work by Archie James and Michael Blombach this years honorees for the award the 40-plus volunteers who helped finish out the projshyect were kept busy and focused so that we could all enjoy our new facilities when AirVenture started

Our sincere admiration and heartfelt thanks to Jim Swol Archie James and Michael Blombach for their hard work Congratulations gentlemen

EAA Share the Spirit Sweepstakes This new Aviat Husky could be yours

Its on The 2010 EAA Share the Spirit Sweepshystakes website is now live and with it your chance to flyaway in the grand prize-a brand new fully equipped Aviat Husky A-1 C To top things off (includshying the 50-gallon fuel tank over and over again) the grand prize comes with a full years worth of fuel credit from Chevron plus 50000 points in Chevrons FlyBuys rewards program Equipped with a Garmin GsOO and GNS 430 panel-mount avionics suite and a set ofWipaire C2200 hydrauliC wheel skis the grand prize Husky will take you places youve never been

But you have to enter and fortunately there are many ways to do so (Entry coupons are included in the November issue of Sport Aviation and will also be included in the 2010 January March and May issues of EAAs flagship magazine) Or you can enter anytime at wwwWinAPlanecom

Other top sweepstakes prizes include a Honda Big Red mUltipurpose utility vehicle REMOS Pilot Center sport pilot training certificate mens Hamilton Khaki X-Wind aviation watch Canon EOS SOD camera kit with lens and Bose Wave music system

VINTAGE AIRPLANE 3

so what would a former high school track star Army Speshycial Ops soldier and parashychute ace want for a vintage aircraft If youre a guy like

Jack Tiffany of Spring Valley Ohio youd go for the most unusual thing you could find-an Autogiro

There was only one problem for the energetic Tiffany a Vietnam vetshyeran now in his seventh decade he couldnt find one to restore Other neat projects came and went for his laid-back confederation of reshystorers that bill themselves as Leadshying Edge Aircraft (liOn the Trailing Edge of Technology is its motto) A Fairchild Kreider-Reisner 21 biplane a Fleet 16B a couple of Davis Dshy1Ws and a smattering of Wacos and other ancient but lovable aircraft passed through the hangar doors but an Autogiro proved elusive He searched for one for 28 years

Enter the third generation of aviashytion fanatics in the Tiffany sphere of influence Jacks father had been an Air Force crew chief and for Jack aviation was a major part of his life Later when he married Kate (an avowed aviation nut herself shes

NOVEMBER 2009

HG fRAUT SCHY

6

served as a volunteer judge at EAA AirVenture Oshkosh) he got a boshynus in the bargain Kates son Nick The young boy soon became as enshyamored as his stepfather with aviashytion and as a teenager Nick became quite the aviation sleuth digging up tidbits of handy aviation knowledge That tenacity would payoff in 1999 when he came to Jack with the reveshylation that there was an Autogiro out there that could be restored In fact there were two

It didnt take long for Jack and Nick to track down Al Letcher of Moshyjave California AI a longtime colshylector of vintage aircraft had bought the remains of a Pitcairn PA-18 from Ted Sowirka who had owned it for 43 years But how it came to be in his hands is a story that will warm the

heart of many a potential restorer who still has hopes of finding his own aeronautical Holy Grail

History The Pitcairn PA-18 Autogiro was

created by the company after the firm had created quite a name for itshyself with the PCA-2 Autogiro a large expensive craft that was bought by a few firms for its novel appearance which since it attracted a lot of atshytention made it a suitable platform for advertising But the PCA-2 with a 300-hp Wright Whirlwind on the nose and a 4S-foot rotor span was a big rotorcraft It could carry three with ease and its hulking presence on the ground made it hard to miss (Autogiro with a capital A is the spelling coined by the Cierva Auto-

Since it is a fixed-spindle system the rotor head is relatively simple The cables and the bungee cords attached to them act as limit stops when the rotor is rotating slowly or is stopped To the sides of the rotorshyattach hinges are the squarish rubshyber pads that in combination with the dampers installed farther out on each blade act to dampen and limit the leadlag movement of each rotor blade as it flies around the rotor disc To the left is the pre-rotator gearbox which engages with the helical spur gear bolted to the bottom of the roshytor head The pre-rotator is used to spin up the rotor blades to a stable rpm before the takeoff roll is started Having a spun-up rotor allows the rotor to be started and brought up to speed without the hazard of taxiing with a low-speed unstable rotor sysshytem and it significantly reduces the takeoff run

By necessity the rotor blades are quite flexible which require the trailing edge of each blade to be segmented This leather patch on the trailing edge covers one of the slip joints on the trailing edge

When running the short stacks on the 160-hp five-cylinder Kinner-R-55 give the Pitcairn a distinctive bark in flight

VINTAGE AIRPLANE 7

After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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Flight Instructor and let me tell you - not only is the personal

hometown family feeling of dealing with AUA wonderful year

after year they find a way to insure my precious airplanes at a

value bar none lower than any other companyI

- Charles Tippet

Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

AUA is Vintage Aircraft Association approved To become a member of VAA call 800middot843middot3612

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Lower premiums with payment options - Additional coverages - Flexibility on the use of your aircraft - Experienced agents Owine quote request available - AUA is licensed in all states

Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

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40 NOVEMBER 2009

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cil of the Mexican Federation of Pishylots (FEMPPA) and are an authorized distributor for INEGI the Mexican charting office which allows us to stay abreast of Mexican aeronautical issues and products

TSA and DHS Merge Border Flight Crossing Procedures

Two Department of Homeland Seshycurity (DHS) agencies recently merged their border security programs to eliminate redundancy as well as the paperwork burden of international travelers The Transportation Secushyrity Administrations (TSA) Internashytional Waiver program will be folded into Customs and Border Protections (CBP) Advanced Passenger Informashytion System (APIS)

This will satisfy a commitment made at AirVenture 2009 by TSAs new general-aviation manager Brian Deshylauter and CBPs APIS program manshyager Eric Rodriguez to improve the border-crossing procedure for generalshyaviation pilots through collaboration The info merger will allow pilots to complete only the CBP electronic APIS paperwork to fly across US borders

EAA which has advocated for a less onerous system has prepared a guide on how to navigate the current reshyquirements until the new process is fishynalized That is available at wwwEAA orgnews20092009-0S-21_cbpasp

VAA Volunteer of the Year Awards

During the fall board meeting Jim Swol (right) was presented with acommemorashytive clock and a certificate commemorating his selection as the 2009 Art Morgan VAA Flightline Volunteer of the Year

Each year the Vintage Aircraft Association honors two of its own for their service to the VAA and its members during the annual convention As it is every year its tough to pick just one person for such an honor but this year was especially challenging as we had afantastic group

of volunteers step it up an extra notch during the months prior to this years amazing event and during the convention

The Art Morgan VAA Flightline Volunteer of the Year comes to us all the way from the state of Maine For years we have both marveled and worried at the willingness of the VAA flightline volunteers to keep going and do whatever was requested of them and Jim Swol epitomizes that volunteer work ethic- always on the spot doing what needs to be done year after year

The VAA Behind the Scenes Volunteer of the Year is actually a twosome this year The wayshybeyond-the-call -of-duty work spearheaded by these two volunteers made it possible for us to comshyplete the Vintage Hangar on time and under budget Thanks to the work by Archie James and Michael Blombach this years honorees for the award the 40-plus volunteers who helped finish out the projshyect were kept busy and focused so that we could all enjoy our new facilities when AirVenture started

Our sincere admiration and heartfelt thanks to Jim Swol Archie James and Michael Blombach for their hard work Congratulations gentlemen

EAA Share the Spirit Sweepstakes This new Aviat Husky could be yours

Its on The 2010 EAA Share the Spirit Sweepshystakes website is now live and with it your chance to flyaway in the grand prize-a brand new fully equipped Aviat Husky A-1 C To top things off (includshying the 50-gallon fuel tank over and over again) the grand prize comes with a full years worth of fuel credit from Chevron plus 50000 points in Chevrons FlyBuys rewards program Equipped with a Garmin GsOO and GNS 430 panel-mount avionics suite and a set ofWipaire C2200 hydrauliC wheel skis the grand prize Husky will take you places youve never been

But you have to enter and fortunately there are many ways to do so (Entry coupons are included in the November issue of Sport Aviation and will also be included in the 2010 January March and May issues of EAAs flagship magazine) Or you can enter anytime at wwwWinAPlanecom

Other top sweepstakes prizes include a Honda Big Red mUltipurpose utility vehicle REMOS Pilot Center sport pilot training certificate mens Hamilton Khaki X-Wind aviation watch Canon EOS SOD camera kit with lens and Bose Wave music system

VINTAGE AIRPLANE 3

so what would a former high school track star Army Speshycial Ops soldier and parashychute ace want for a vintage aircraft If youre a guy like

Jack Tiffany of Spring Valley Ohio youd go for the most unusual thing you could find-an Autogiro

There was only one problem for the energetic Tiffany a Vietnam vetshyeran now in his seventh decade he couldnt find one to restore Other neat projects came and went for his laid-back confederation of reshystorers that bill themselves as Leadshying Edge Aircraft (liOn the Trailing Edge of Technology is its motto) A Fairchild Kreider-Reisner 21 biplane a Fleet 16B a couple of Davis Dshy1Ws and a smattering of Wacos and other ancient but lovable aircraft passed through the hangar doors but an Autogiro proved elusive He searched for one for 28 years

Enter the third generation of aviashytion fanatics in the Tiffany sphere of influence Jacks father had been an Air Force crew chief and for Jack aviation was a major part of his life Later when he married Kate (an avowed aviation nut herself shes

NOVEMBER 2009

HG fRAUT SCHY

6

served as a volunteer judge at EAA AirVenture Oshkosh) he got a boshynus in the bargain Kates son Nick The young boy soon became as enshyamored as his stepfather with aviashytion and as a teenager Nick became quite the aviation sleuth digging up tidbits of handy aviation knowledge That tenacity would payoff in 1999 when he came to Jack with the reveshylation that there was an Autogiro out there that could be restored In fact there were two

It didnt take long for Jack and Nick to track down Al Letcher of Moshyjave California AI a longtime colshylector of vintage aircraft had bought the remains of a Pitcairn PA-18 from Ted Sowirka who had owned it for 43 years But how it came to be in his hands is a story that will warm the

heart of many a potential restorer who still has hopes of finding his own aeronautical Holy Grail

History The Pitcairn PA-18 Autogiro was

created by the company after the firm had created quite a name for itshyself with the PCA-2 Autogiro a large expensive craft that was bought by a few firms for its novel appearance which since it attracted a lot of atshytention made it a suitable platform for advertising But the PCA-2 with a 300-hp Wright Whirlwind on the nose and a 4S-foot rotor span was a big rotorcraft It could carry three with ease and its hulking presence on the ground made it hard to miss (Autogiro with a capital A is the spelling coined by the Cierva Auto-

Since it is a fixed-spindle system the rotor head is relatively simple The cables and the bungee cords attached to them act as limit stops when the rotor is rotating slowly or is stopped To the sides of the rotorshyattach hinges are the squarish rubshyber pads that in combination with the dampers installed farther out on each blade act to dampen and limit the leadlag movement of each rotor blade as it flies around the rotor disc To the left is the pre-rotator gearbox which engages with the helical spur gear bolted to the bottom of the roshytor head The pre-rotator is used to spin up the rotor blades to a stable rpm before the takeoff roll is started Having a spun-up rotor allows the rotor to be started and brought up to speed without the hazard of taxiing with a low-speed unstable rotor sysshytem and it significantly reduces the takeoff run

By necessity the rotor blades are quite flexible which require the trailing edge of each blade to be segmented This leather patch on the trailing edge covers one of the slip joints on the trailing edge

When running the short stacks on the 160-hp five-cylinder Kinner-R-55 give the Pitcairn a distinctive bark in flight

VINTAGE AIRPLANE 7

After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

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Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

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40 NOVEMBER 2009

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Page 5: VA-Vol-37-No-11-Nov-2009

so what would a former high school track star Army Speshycial Ops soldier and parashychute ace want for a vintage aircraft If youre a guy like

Jack Tiffany of Spring Valley Ohio youd go for the most unusual thing you could find-an Autogiro

There was only one problem for the energetic Tiffany a Vietnam vetshyeran now in his seventh decade he couldnt find one to restore Other neat projects came and went for his laid-back confederation of reshystorers that bill themselves as Leadshying Edge Aircraft (liOn the Trailing Edge of Technology is its motto) A Fairchild Kreider-Reisner 21 biplane a Fleet 16B a couple of Davis Dshy1Ws and a smattering of Wacos and other ancient but lovable aircraft passed through the hangar doors but an Autogiro proved elusive He searched for one for 28 years

Enter the third generation of aviashytion fanatics in the Tiffany sphere of influence Jacks father had been an Air Force crew chief and for Jack aviation was a major part of his life Later when he married Kate (an avowed aviation nut herself shes

NOVEMBER 2009

HG fRAUT SCHY

6

served as a volunteer judge at EAA AirVenture Oshkosh) he got a boshynus in the bargain Kates son Nick The young boy soon became as enshyamored as his stepfather with aviashytion and as a teenager Nick became quite the aviation sleuth digging up tidbits of handy aviation knowledge That tenacity would payoff in 1999 when he came to Jack with the reveshylation that there was an Autogiro out there that could be restored In fact there were two

It didnt take long for Jack and Nick to track down Al Letcher of Moshyjave California AI a longtime colshylector of vintage aircraft had bought the remains of a Pitcairn PA-18 from Ted Sowirka who had owned it for 43 years But how it came to be in his hands is a story that will warm the

heart of many a potential restorer who still has hopes of finding his own aeronautical Holy Grail

History The Pitcairn PA-18 Autogiro was

created by the company after the firm had created quite a name for itshyself with the PCA-2 Autogiro a large expensive craft that was bought by a few firms for its novel appearance which since it attracted a lot of atshytention made it a suitable platform for advertising But the PCA-2 with a 300-hp Wright Whirlwind on the nose and a 4S-foot rotor span was a big rotorcraft It could carry three with ease and its hulking presence on the ground made it hard to miss (Autogiro with a capital A is the spelling coined by the Cierva Auto-

Since it is a fixed-spindle system the rotor head is relatively simple The cables and the bungee cords attached to them act as limit stops when the rotor is rotating slowly or is stopped To the sides of the rotorshyattach hinges are the squarish rubshyber pads that in combination with the dampers installed farther out on each blade act to dampen and limit the leadlag movement of each rotor blade as it flies around the rotor disc To the left is the pre-rotator gearbox which engages with the helical spur gear bolted to the bottom of the roshytor head The pre-rotator is used to spin up the rotor blades to a stable rpm before the takeoff roll is started Having a spun-up rotor allows the rotor to be started and brought up to speed without the hazard of taxiing with a low-speed unstable rotor sysshytem and it significantly reduces the takeoff run

By necessity the rotor blades are quite flexible which require the trailing edge of each blade to be segmented This leather patch on the trailing edge covers one of the slip joints on the trailing edge

When running the short stacks on the 160-hp five-cylinder Kinner-R-55 give the Pitcairn a distinctive bark in flight

VINTAGE AIRPLANE 7

After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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bull Pilot for over 25 years

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bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

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DIRECTORS Steve Bender Jeannie Hill

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chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

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40 NOVEMBER 2009

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Page 6: VA-Vol-37-No-11-Nov-2009

served as a volunteer judge at EAA AirVenture Oshkosh) he got a boshynus in the bargain Kates son Nick The young boy soon became as enshyamored as his stepfather with aviashytion and as a teenager Nick became quite the aviation sleuth digging up tidbits of handy aviation knowledge That tenacity would payoff in 1999 when he came to Jack with the reveshylation that there was an Autogiro out there that could be restored In fact there were two

It didnt take long for Jack and Nick to track down Al Letcher of Moshyjave California AI a longtime colshylector of vintage aircraft had bought the remains of a Pitcairn PA-18 from Ted Sowirka who had owned it for 43 years But how it came to be in his hands is a story that will warm the

heart of many a potential restorer who still has hopes of finding his own aeronautical Holy Grail

History The Pitcairn PA-18 Autogiro was

created by the company after the firm had created quite a name for itshyself with the PCA-2 Autogiro a large expensive craft that was bought by a few firms for its novel appearance which since it attracted a lot of atshytention made it a suitable platform for advertising But the PCA-2 with a 300-hp Wright Whirlwind on the nose and a 4S-foot rotor span was a big rotorcraft It could carry three with ease and its hulking presence on the ground made it hard to miss (Autogiro with a capital A is the spelling coined by the Cierva Auto-

Since it is a fixed-spindle system the rotor head is relatively simple The cables and the bungee cords attached to them act as limit stops when the rotor is rotating slowly or is stopped To the sides of the rotorshyattach hinges are the squarish rubshyber pads that in combination with the dampers installed farther out on each blade act to dampen and limit the leadlag movement of each rotor blade as it flies around the rotor disc To the left is the pre-rotator gearbox which engages with the helical spur gear bolted to the bottom of the roshytor head The pre-rotator is used to spin up the rotor blades to a stable rpm before the takeoff roll is started Having a spun-up rotor allows the rotor to be started and brought up to speed without the hazard of taxiing with a low-speed unstable rotor sysshytem and it significantly reduces the takeoff run

By necessity the rotor blades are quite flexible which require the trailing edge of each blade to be segmented This leather patch on the trailing edge covers one of the slip joints on the trailing edge

When running the short stacks on the 160-hp five-cylinder Kinner-R-55 give the Pitcairn a distinctive bark in flight

VINTAGE AIRPLANE 7

After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

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Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

II have been flying now for over 25 years I am a Certified

Flight Instructor and let me tell you - not only is the personal

hometown family feeling of dealing with AUA wonderful year

after year they find a way to insure my precious airplanes at a

value bar none lower than any other companyI

- Charles Tippet

Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

AUA is Vintage Aircraft Association approved To become a member of VAA call 800middot843middot3612

Aviation insurance with the EAA Vintage Program oHers

Lower premiums with payment options - Additional coverages - Flexibility on the use of your aircraft - Experienced agents Owine quote request available - AUA is licensed in all states

Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

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Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

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VINTAGE AIRPLANE 39

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After arriving in Jim Hammonds shop the Pitcairns pieces were assembled as much as possible so the restorers could get a better idea of just what they had

A restorable PA-18 rotor head and pre-rotator gearbox was obtained from Steve Pitcairn and thanks to his intershyest in his fathers company history Steve was also able to supply a set of drawings so Phil Riter could build a new rotor mast

The rotors were complete with steel spars that were After 60-plus years its not surprising that the blade rubshy inspected and deemed airworthy All-new wood comshyber dampers were not usable so a new set were cast usshy ponents were used to restore the blades With the expeshying new urethane rubber material with the correct 90 rience of building the first set the Leading Edge gang durometer hardness

giro Company for aircraft produced under license the generic termaushytogyro applies to all rotary-winged aircraft with unpowered rotors the FAA simply avoids the entire issue by calling them gyroplanes)

What was also needed was a smaller more compact version something that a well-heeled owner could purchase and fly Harold Pitshycairn the founder of the aviation manufacturing concern that bore his family name had started his firm in the 1920s building mail-hauling aircraft renowned for their strucshytural strength and safety with regard to their ability to protect the pilot in the event of a crash Harolds longshytime pursuit of the safe operation

NOVEMBER 2009

continued to build blades as spares

of aircraft led him to a collaborative agreement between his company and Juan de la Cierva the inventor of the Autogiro Assigned the exclushysive rights to license and produce the Autogiro in the United Sates the Pitcairn-Cierva Autogiro Company of America pursued the vision of a safe aircraft that could be landed just about anywhere

Harold Pitcairn wanted that cashypability to be within reach of anyshyone who could fly and a personal aircraft was just the next logical step in the progression of the Autogiro The first version the PAA-l was bashysicallya scaled-down PCA-2 with a fixed-spindle rotor system atop a fuselage powered by a 125-hp Kinshy

nero One version was built with the Chevrolair engine and an odd tail wheelnose wheel configuration

The PAA-1 was well-received but it was considered significantly unshyderpowered (25 were built and deshylivered in the darkest period of the Great Depression of the early 1930s) but it wasnt exactly what Harold wanted The factory came up with the next version a slightly larger aircraft that was destined to be just what Harold Pitcairn wanted In fact he liked it so well that in 1932 when he rented a beach house on the Jersey shore he used his pershysonal PA-18 as his weekend comshymuter car to cover the 80-mile drive in half an hour rather than battling

8

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

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Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

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VINTAGE AIRPLANE 39

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Page 8: VA-Vol-37-No-11-Nov-2009

Fifty-four individual ribs are in each blade for a total of 216 ribs in each set of four blades Each was routed out using a CNC machine and then the ribs are secured to the tubular steel spar using bolts and a flange

Since the original wood parts were sigshynificantly deteriorated after being stored outside for many years they needed a complete restoration A major portion of the wing and aileron rebuild was done by Jan Lavally

the terrestrial traffic down below Landing on the beach in front of the cottage proved to be a simple matter and tucking it neatly on the sand nearby kept it ready for a dash back to his office near Philadelphia

The PA-18 was also popular with new rotorcraft aficionados deliveries began in 1932 with 18 being built (Nineteen serial numbers are listed in Joe Juptners US Civil Aircraft but it is believed that one airframe had two serial numbers in its lifetime) Debuting at the Detroit Air Show for a price of $4940 the new Autogiro had improved performance thanks in part to engineering work that reshyfined the rotor head allowing for smoother rotor operation and the

ANTIQUE ALERT NOTICE Followtnc are excerpt lrom II letter ptq ttal lDfol1llAllim em PltcaJro Autoclro rHI demiddot Mn II better end1namp than the letter lDdieatee

Eado_eeI au aom ahot of poor Util PltcairD autolYlo (PA-lO 1 thUlk) aUtill aftd roULDa aay at Lupora P ylvul lAto 011 it OWII ate la 1I0t available howav l vamp bbullbulln told WI V Zaadt OWD th ptabullbull aDd h_ the rototored aombullbulllIar n ahport h b old and that mI1amp the poulblU 01 omeoa comllli alonl with the lIaual bulldr atKI r1llUbl oval amparytbllli ill uy nare ua not maay Iyro lut tod ay and W 011amp Is oJth bullbullrinl 1 ha alao bullbullnt t of photo to Harry Lounabury of the ~rtcampQ HeUcopshytar Soctay with the bullbullma plbullbull to pray_I _antozr dbullbulltructiOIl Ott hl~ric aherdt 1 do aot bow hti clrcunutaac amprOund Wa plaa tlt o_ur may be tryial to Pl it la b~ but peopl at Lb nld did 80t at m that hnprbullbullbulltoa

Warna D Shipp 812 CroIfD Stre Brooklye 11 N Y

In 1954 Warren Shipp had spotted the forlorn Pitcairn sitting at a Pennshysylvania airport Two of his photos and a brief write-up pleading its case were published in the first issue of American Airman magazine

increase in horsepower to 160 pumped out by a Kinner R-5 engine It still had a fixed-spinshydle rotor system which meant that all control of the aircraft was affected using aerodynamic controls that is rudder elevashytor and ailerons mounted on the stub wings Direct control of the rotor head was being acshytively worked on at this point but it would be months before the system was perfected so that it would allow the dispensing of the stub wings

In March of 1932 serial number G-65 the fourth PA-18 off the factory line was delivshyered as the personal aircraft of

the company preSident and it was also used as a factory demonstrator Harold Pitcairn had a great deal of affection for the little Autogiro as evidenced in a portion of a letter he sent to his executive vice president Geoff Childs Sunday the weather became very bad so I told Chambliss to take my machine over to the hanshygar Because of the wind direction he was going to take off towards the Church The ground was slippery and the machine was on a slope He got into the air before he meant to and the starter was engaged This in addition to all the other conditions under which he was working made the machine turn and drift very badly to the right Before he had

the situation straightened out he hit the fence so that my little giro is minus a set of blades When I came out of Church it was standing up on its nose I patted it gently and all it said was cheep cheeplII

He wouldnt be the first pershyson taken in by the charms of the little Autogiro This particular PAshy18 registered as NC12678 was kept by Harold until it was sold in 1935 Anne West Strawbridge was an adventuresome spirit who had climbed mountains and was an acshycomplished artist and author (A little side note-on the Web and in other publications an incorrect connection was made between Miss Strawbridge and the Strawbridge amp Clothier department store fortune In fact according to her great grandshynephew she was the daughter of a doctor from Maine whose family connection to the department story family is very distant at best She was not the daughter of someone directly related to the store)

Her family fortune allowed her to pursue all sorts of interesting purshysuits Apprehensive about flying she became a convert to the Autogiro after a flight demonstration even after her first PA-18 was crashed by another pilot hitting wires near Wings Field in Philadelphia and killshying the pilot and his passenger In 1935 she bought NC12678 To exshypress her appreciation she sent a

VINTAGE AIRPLANE 9

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 9: VA-Vol-37-No-11-Nov-2009

letter to Harold that read in part Please may I tell you something

of the great pleasure youve given me in allowing me to buy the blue autogiro it was most awfully good of you and Mr Ray to take so much trouble in arranging it and I thank you ever so much I am also writing Mr Ray The giro is the loveliest ship Ive ever flown in and I simply have not words to tell you how much it

10 NOVEMBER 2009

means to me to have her There is a beauty of existence

which one enters through flying the autogiro which is largely a thing of the spirit and could so easily be lost through any discourse (I know you will understand what I express so inshyadequately) but at both factory and flying field one meets only with the most courteous kindness efficiency and a vast love of the work and loyshy

alty to you May I congratulate you on your splendid workz

It seemed the little PA-18 had once again cast its magic spell on yet another aviator Anne Strawbridge came to name the autogiro Isobella In 1936 and 1937 she sent similarly complimentary letters to Harold Pitshycairn expressing her admiration for Isobella and for the instruction beshying provided by Mr Lukens one of

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

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VINTAGE AIRPLANE 39

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Page 10: VA-Vol-37-No-11-Nov-2009

Pitcairns instructor pilots She flew the blue giro more than 90 hours by mid-1937 enjoying the operashytional peace of mind that the Autoshygiro gave her She wrote later

I have been amazed at Mr Lukens ability as an instructor When he took me on I could not have been a more unpromising stushydent Now I get into the ship as transhyquilly as into my Ford car-and with

a lot less feeling of risk in the air than on the highway3

A couple of explanations are in orshyder The color as described to me by Carl Gunther the archivist of the Pitshycairn Aircraft Association was dark blue with a light blue stripe with a white keyline around the stripe

The Mr Ray she refers to in the letter is Jim Ray Pitcairn-Cierva Aushytogiro Companys vice president

and one of the most accomplished Autogiro pilots in history

While there is fascinating mateshyrial to learn more about in Autoshygiro history we need to skip a few years ahead to complete the hisshytory of NC12678 Its 1939 and thanks to the German U-boat menshyace the British are having a devil of a time getting their war effort and nation supplied via convoy across the North Atlantic Looking at any means at their disposal to gain an advantage in knowing where the U-boats were lurking the British contracted with the Pitcairn-Larsen Autogiro Company a successor to the original company set up by Harshyold Pitcairn to remanufacture the remaining PA-18s into sub-spotting Autogiros that could operate from small decks on ships within the conshyvoys Using the PA-18 as a base gave them a quick start on the creation of an Autogiro suitable for the purpose

Technological advances in rotor and flight control systems includshying the now perfected direct-control rotor head gave the remanufactured aircraft now called the PA-39 imshyproved performance and the inshystallation of a 16S-hp Warner Super Scarab gave it added reliability All the company had to do was buy back the remaining PA-18 Autogiros from the owners run them through the remanufacturing process and then load them on ships for delivery to the United Kingdom Thats just what they did with all of them All of them except one Anne West Strawshybridges Autogiro wasnt on the list

Theres no record of what convershysation or letter transpired between the company and Anne Strawbridge but based on her lovely letters to Harshyold Pitcairn I cant imagine it was anything but a very polite 0h my goodness no I could never sell it type of refusal to sell little Isabella so that it go off to war In any event it was not part of the group to be conshyverted to the PA-39 configuration

Her strong attachment to the little blue Autogiro is what saved it for resshytoration many years later only two of the PA-39 Autogiros ever made it

VINTAGE AIRPLANE 11

to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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to England Three were lost at sea in a torpedoing of the cargo ship carryshying them with at least one remainshying in the States where it was used for research and development work There is one PA-39 remaining reshystored and on display in EAAs Pitshycairn Hangar on Pioneer Airport a gift of Harold Pitcairns son Stephen

After civilian flying was banned for the duration of the war along the East Coast Anne never again flew her beloved giro She died in 1941 at the age of 58 willing the little rotorcraft to her brother John Strawbridge

A few years later just after the end of World War II the ownership of the Autogiro flipped back and forth a few times before being sold to GampA Aircraft It was Wind-damaged and later Firestone Aircraft (the successor to GampA Aircraft) repaired it

They didnt keep it long (GampA also operated the remaining PA-39) sellshying it to Sky Voice Inc of East Orshyange New Jersey on March IS 1947 A shoreline advertising company Sky Voice planed to pull banners and even put a big speaker in the giro to generate advertising publicity Theres no record it actually did that with the Autogiro but its fun if not

12 NOVEMBER 2009

a bit unnerving to imagine a voice from the sky exhorting those on the shore to Eat at Joes

Four years later the Wyoming Valley School of Aviation at WilkesshyBarre Pennsylvania acquired the Autogiro after Joseph Budjinski of the school determined by queryshying the Civil Aviation Authority the most recent registered owner Within the next two years the school folded and on July 3 1954 a flight school on the same field Morlin Air Service sold NC12678 to Ted Sowirka who brought the still mostly complete giro to Old Star Airport near Langhorne Pennsylshyvania Most likely it was sold by the flight school as part of a settlement for payment and while such things happen if theyre not executed properly it can cause a big headache for those who follow as well see later in this article

While the rotor blades were stored in a hangar the partially reshyworked fuselage sat outside While it was there Warren D Shipp a transit policeman from New York City who had an interest in aviation and Aushytogiros in particular spotted it sitshyting out in the grass Shipp one of

the earliest American Aviation Hisshytory Association members (No 14) sent a couple of photos and a letter that were published in the first issue of American Airman magazine (Sepshytember 1957) imploring someone to save the Autogiro before it was lost to history That story helped Nick Hurm track down the whereshyabouts of the PA-18 (See the photo in this article)

Sometime later after those phoshytos were taken a rogue pilfered the main rotor mast supporting strucshyture and the all-important rotor head and pre-rotator mechanism forcing the Autogiros storage inside a hangar Ted still intended to reshystore the aircraft to flying condition but without the heart of the aircraft it proved to be a long-term storshyage situation While he never got a chance to restore it Ted Sowirkas dedication to keeping the project as intact as possible saved it for the next generation of restorers

By 1996 the registration of the aircraft has been allowed to lapse and the N number has been assigned to a Cessna 172 made in 1973 Ted had attempted to get the aircraft reshyregistered noting in a letter to the

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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VINTAGE AIRPLANE 37

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 12: VA-Vol-37-No-11-Nov-2009

agency dated July 1996 that Nearly everything else on the aircraft has been stored the AutOgiro could be built if by me since 1954 drawings could be obtained

The next month Ted sold but the rotor head isnt someshythe project to Al Letcher of thing one can just whip out Mojave California The next using a band saw and a lathe year Nick Hurm tracked Thankfully Jack had been in the PA-18s whereabouts regular contact with Steve Pitshyto Al Letcher Jack Tiffany cairn Harold Pitcairns son first made contact with AI and a well-known restorer checking to see if Al would and aviation enthusiast be willing to part with the Steve had participated in and Autogiro Over the next two funded the restoration of the

Pilot Andrew King gathered as much written mateshyyears during a visit to Calshy most famous of Pitcairn Autoshyrial as he could regarding flying the PA-18 along withifornia by Jack he made a giros the PCA-2 Miss Chamshyspending considerable time interviewing both Steve deal to restore the Autogiro pion and he had a spare PA-18 Pitcairn and Johnny Miller who both had extensive for Al Letcher As agreed type rotor head that he was experience flying Pitcairn Autogiros during the restoration Jack willing to sell Steve also had

was also going to create a access to a few of the drawshyclone of the Autogiro Jack ings from the company so he giddy with the prospect just Still you dont know what you was able to fill in the blanks couldnt keep quiet about for a few of the missing parts the find and word leaked dont know and not everything that including the all-important out during the annual EAA fly-in convention that there was available back in 1931 had was indeed a Pitcairn out there to be restored Not too surfaced in 2008 much later Jack heard from Al that instead of allowing Jack to restore the PA-18 Al has deshycided to sell the ship to another vinshytage airplane enthusiast

Jack forthrightly explained that he didnt think that was fair and that he should have the right of first refusal on the purchase After thinkshying for a moment Al agreed Jack then said I want it and shortly thereafter hung up the phone happy that hed come to an agreeshyment to buy the Autogiro He hung up a bit too quickly it turned out When Kate asked him how much it was going to cost it suddenly struck Jack that he didnt know He jumped back on the phone heard a price gulped and hung up When the subject of the price came up again with Kate after the call his reshysponse was in part Well if we sell the house the cars

Thankfully that draconian meashysure wasnt needed Longtime friend and fellow aircraft restorer Jim Hamshymond whose family owns and opshyerates Hammond DrieRite in Xenia Ohio became a silent partner in the

project by helping with the funding to acquire the Autogiro Within days a truck and crew consisting of Jack and Kate Tiffany Herman Leffew Don Siefer and Herb Ware were off to the Mojave Desert to pick up the remains of the rotorcraft still missshying the parts stolen from it so long ago By Thanksgiving of 1999 it was in Jim Hammonds shop where Jim put all the pieces they had dragged back to Ohio into a semblance of an Autogiro Soon it was moved to the Leading Edge shops near Dayshyton The restorers had high hopes of finishing the aircraft by the end of 2003 just in time for the 100th anniversary of the Wright brothers powered flights in Kitty Hawk But not surprisingly given the multi shyfaceted issues involved that date would come and go before the PAshy18 was ready to fly

The Restoration As I mentioned before the projshy

ect was mostly complete but it did lack one critical item the rotor head

main rotor mast Phil Riter a master at sheet metal work and welding created the new mast and did all of the sheet metal work for the cowling including the beautiful nose-

bowl covering the Kinner What often appear to be little

changes in a type design often wind up being big headaches Somewhere along the line the little blue Autogishyros Kinner R-5 engine was separated from the airframe and it wasnt part of the project when it was brought to Ohio Thats fine a Kinner R-5 is rare to begin with but the later version the Kinner R-55 is more common having been used on the Ryan PTshy22 Theyre nearly identical with the R-55 having a number of improve shyments that make it a more reliable enshygine so making the change shouldnt be too much of a big deal right

Not so fast in this case since the R-55 isnt on the type certificate data sheet installing it means that the reshystorers were making a major alterashytion to the aircraft Just getting all the data and approvals through the enshygineering section of the FAA added more time than they expected to the project Like most every Kinner rework done these days the Kinner was inspected and overhauled by Kin-

VINTAGE AIRPLANE 13

Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

II have been flying now for over 25 years I am a Certified

Flight Instructor and let me tell you - not only is the personal

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after year they find a way to insure my precious airplanes at a

value bar none lower than any other companyI

- Charles Tippet

Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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3 8 NOVEMBER 2009

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

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VINTAGE AIRPLANE 39

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Theres plenty more photos

and other goodies on the Pitcairn at wwwvintageaircrafimiddotorglextraslpitcairn

ner engine experts AI and Brad Ball in Santa Paula California

The other obviously critical items were the main rotor blades Each of the blades as can be seen in the photos accompanying this article are built like a very high-aspect rashytio wing with a steel tube spar over which are fitted tightly spaced wood ribs with plywood leading edges and stainless steel trailing edges One un-

After a fun crossshycountry from New Carlisle Ohio to Oshkosh the PA-18 Autogiro spent the summer months displayed in EAAs Pitcairn Hangar located behind the museum at EAAs Pioneer Airport

usual aspect to their construction is the requirement for slip joints in the trailing edge of each blade necesshysary since the blades flex significantly in flight This flexing is important soaking up both flight and structural loads spanwise along the blades as each blade Circumnavigates the roshytor arc 140 times per minute just a little faster than twice each second The rotor blades that had been reshytained with the project were in rough shape but the spars were usable alshylowing the restorers to build up not only the ribs (all 216 for a set of four blades thank goodness for CNC millshying machines) but they had enough information and parts to create a new replacement set of rotor blades and are confident that their rotor shop can handle their maintenance needs for years to come

The rest of the rotorcrafts restorashytion was pretty straightforward with the standard repairs being made to a 70-plus-year-old airframe While the

stub wings were intact they were reshybuilt almost completely built up enshytirely of wood The fuselage needed a bit of steel tubing replaced and while we ll get a bit ahead of the story a bit here one little bit of clever engineershying deserves to be highlighted During the flight-testing phase of the restored Pitcairn a series of mistakes resulted in a main rotor blade or two or three contacting the top of the vertical fin It promptly folded over to the side with no damage done to the tail post or the rest of the fuselage (Youll get a chance to read more about the incident in the upcoming January 2010 issue of EAA Sport Aviation in the feature article on the PA-18 written by Andrew King)

Once repairs were started the reashyson why the fin folded so neatly beshycame apparent Pitcairns engineers realizing that it was likely that a comshybination of surface winds low-rotor rpm and taxiing on the ground could result in a rotor strike in the fin simshyply had a set of holes drilled in the tail post creating a weaker spot on the tube just above the top of the fuseshylage Whack it with a rotor blade and voila the fin flips to the side damage is minimal to the fuselage and if you were a lucky owner back then you could call up the factory and order up a new fin If youre a restorer you get to break out your jig and torch and build up a new one yourself

The Wright brothers anniversary in 2003 came and went and the projshyect wasnt done yet but restorers were

making good progress and it looked like the middle of the first decade might see it flying But as we all know sometimes what you plan isnt what happens Paperwork on the repairs and alterations was taking time as was the process of acquiring the use of the orig-

Notes 1 Chapter 5 page 171 Harold F Pitcairn Aviator Inventor and Developer of the Autogiro by Carl R Gunther published by Bryn Athyn College Press 2 Chapter 8 pages 330331 see above 3 Ch apter 8 page 381

14 NOVEMBER 2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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Flight Instructor and let me tell you - not only is the personal

hometown family feeling of dealing with AUA wonderful year

after year they find a way to insure my precious airplanes at a

value bar none lower than any other companyI

- Charles Tippet

Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

AUA is Vintage Aircraft Association approved To become a member of VAA call 800middot843middot3612

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Lower premiums with payment options - Additional coverages - Flexibility on the use of your aircraft - Experienced agents Owine quote request available - AUA is licensed in all states

Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

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Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 14: VA-Vol-37-No-11-Nov-2009

inal N the side of a~~~tLy 172 Jack (an ter of fact) did his hp(1tSIt-rrn

owner that it would be ated if the original N number moved back to the Pitcairn Jack pay to have the 172 repainted with bullbull~bers a that

ith th

w a 0

see the restoration fly Johnny Miller who had flown his own PCA-2 across the United States a full two weeks before Amelia Earharts flight in the Beech-Nut gum-sponsored PCA-2 had been regularly consulted about flying the Autogiro by Andrew King who was slated to be the Pitcairns pilot Johnny died on June 24 2008 within days of when the first flights were scheduled And Steve Pitcairn who had done so much to help the Leadshying Edge crew passed away a couple of months before in March of 2008 Andrew King in particular was thankshyful that hed had the good fortune of knowing and chatting with both men about the operation of the Autogiro

Nearly three years of time was added to the restoration due to one significant paperwork issue-accordshy

ing to the FAA records the last regisshytered owner was Sky Voice The next

didnt actually execute a bill of for the aircraft which meant that

FAAs eyes Jack and Leading didnt have a clean pashy

establish ownership Three npmiddotlATfL- heck ensued for

~~~~~ crew fithe rest

es during Autogiro operation middot period of time from when the or brake is reshyleased and when the rotor has enough speed for centrifugal force and lift to keep the blades steady in their respecshytive flight paths as they whirl around the rotor disc During early testing Andrew was moving down the runshyway at low rotor rpm when he heard the main rotor blades smack the top of the vertical fin The blades werent damaged but the fin was neatly laid over the built-in fail point having done its job perfectly Not too much later an old checklist surfaced that pointed out that no movement of the giro should be done unless the roshytors are stopped or unless the rotor is turning at least 6S rpm

Three weeks later after repairs were

made nine years of work more than 6000 man-hours of restoration time and untold mechanical difficulties and paperwork hassles were about to melt away as mid-summer dawned with light winds and just a few cirrus clouds way up in the heavens

Andrew and the Autogiro were ready on J with a that

ucky see just ore Pitca giro flying as

the Posey brothers work toward the completion of the only other PA-18 known to exist but for me and my son Alden along with EAA photogshyrapher Bonnie Kratz and out photo pilot Janet Davidson the sight of the Pitcairns slowly turning blades rotatshying over Andrews head as he slingshywinged his way north to Oshkosh past more than 100 newly constructed wind turbines firmly anchored to the ground will be something well never forget Its a remarkable aircraft crafted and engineered by some of the finest engineers of the first half of the previous century and restored by an equally talented group of men and women who are thrilled to have been given the opportunity to restore one of aviations great aircraft the Pitcairn AutOgiro

VINTAGE AIRPLANE 15

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 15: VA-Vol-37-No-11-Nov-2009

Steve Pitcairn wipes down Miss Champion after arrival at Oshkosh 86

But few aircraft caught and held the public attention as did the Aushytogiro Called flying windmills by news reporters who had little understanding of the principles of autorotational flight these strangeshylooking aircraft invented by a Spanish engineer named Juan de la Cierva captured the hearts and minds of the air-minded public beshycause of their remarkable perforshymance coupled with a high degree of safety These facts made Autoshygiros an ideal means to carry out nationwide advertising campaigns by a number of American manufacshyturers The Champion Spark Plug Company was one of these

Champion executives were not slow to see the large amount of publicity Autogiros drew wherever they performed across the country Nor was the fact that many of the leaders of American aviation such as Charles Lindbergh Jimmy Dooshylittle Frank Hawks Amelia Earhart Clarence Chamberlin David Inshygalls and many others were beatshying a steady path to Pitcairn Field

near Willow Grove Pennsylvania where Harold Pitcairn was designshying and building these phenomeshynal aircraft

It wasnt long before Champion Vice President Me Dewitt showed up at the Pitcairn Aircraft Comshypany office prepared to do busishyness Pitcairn Vice President Edwin Asplundh promptly led Dewitt out to the ramp in front of the main hangar doors where stood an Aushytogiro with its engine idling In the rear cockpit sat Jim Ray Pitcairns chief test pilot who motioned Deshywitt to climb into the front seat As soon as Dewitts safety belt was fastened Jim engaged the clutch bringing the rotor up to flight speed and executed a short steep takeoff within the confines of the fenced-in ramp area

The demonstration of the Aushytogiros characteristics to which Jim treated Dewitt included the usual aerial maneuvers and then a throttled-back pass at the field a mere 15 feet above the grass at a speed of less than 30 miles per

hour yet under complete control and finally a vertical dead-stick landing from 500 feet on the exact spot from where they had departed 10 minutes earlier with a roll of only 2 or 3 feet Dewitt who was no stranger to flying climbed out on the wing as soon as the engine stopped and with a big grin on his face said Im impressed but can our pilot do that Who is your pilot Jim asked Capt Lewis A Yancey if he can handle it reshyplied Dewitt I know Yancey said Jim Hell do fine

As a matter of fact Lon Yancey famed for his trans-Atlantic flight in a Bellanca in 1929 to Rome itshyaly had already been receiving Aushytogiro flight instruction from Jim and Skipper Lukens another Pitshycairn pilot for several days His handling of the Autogiro was quite acceptable With more experience he became an accomplished Aushytogiro pilot with the capability of handling the routines Autogiro demonstrations called for

Satisfied Dewitt signed the sales

VINTAGE AIRPLANE 17

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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after year they find a way to insure my precious airplanes at a

value bar none lower than any other companyI

- Charles Tippet

Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

AUA is Vintage Aircraft Association approved To become a member of VAA call 800middot843middot3612

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Lower premiums with payment options - Additional coverages - Flexibility on the use of your aircraft - Experienced agents Owine quote request available - AUA is licensed in all states

Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 16: VA-Vol-37-No-11-Nov-2009

The markings were accurately reproduced from the original fabric except for Steves name at the rear cockpit

agreement On paper the agreeshyment simply states that in conshysideration of the sum of $15125 in hand paid we hereby sell and transfer unto Champion Spark Plug Company of Toledo Ohio one Aushytogiro type PCA-2 Serial Number 8-27 Engine 12563 engine type Wright Whirlwind J-6 R-975 300 hp Dept of Commerce number NC1l609 manufactured June 1931 free and clear of liens and encumshybrances of whatever kind or nature this 29th day of June 1931 The signatures of Asplundh and Dewitt appeared beside their respective company names and titles

Thus was born Miss Chamshypion-the first rotary-wing aircraft ever selected to lead the Ford Air Tour Two days after the Autogishy

18 NOVEMBER 2009

ros delivery at Toledo Ohio Capt Yancey took off from Ford Airport with the 1931 National Air Tour The Champion Autogiro was the official tour ship During the tour Miss Champion visited 21 states and 38 cities and towns from London Ontario Canada to New Orleans Louisiana and from Fort Worth Texas to Kalamazoo Michigan Total mileage was well in excess of 6500 with her flight log showing more than 120 hours aloft Everyshywhere the Autogiro landed it atshytracted wide attention and easily won the major share of newspaper and radio coverage a fact that visishybly annoyed a number of the other pilots on the tour

After the air tour the Champion company put Miss Champion to

work getting publicity for Chamshypion dealers from Maine to Florida Her demonstrations of controlled slow flight unusual maneuverabilshyity and near vertical landings at the annual National Air Races brought national recognition to this new and safer form of flight

In January of 1932 Miss Chamshypion made a flight considered risky for any aircraft let alone an Autogiro Until then no Autoshygiro had ever flown more than 25 miles over water On January 24 Capt Yancey flew the Autogiro from Miami to Havana Cuba a distance of more than 300 miles His arrival in Havana was greeted by enthusiastic crowds and he was invited to the presidential palace by President Machado

But Yancey had even greater amshybitions A wire to the Pitcairn Autoshygiro Company brought him a week later a specially designed auxiliary fuel tank that he mounted in the front cockpit of his PCA-2 thus doubling his fuel supply He then successfully began his most miracushylous flight of all from Havana over the Cuban wilderness across the wide and treacherous waters of the Yucatan Channel (part of the Gulf of Mexico) and over the trackless expanse of the Yucatan jungles to its capital of Merida a nonstop trip of nearly 500 miles where he was welcomed by the governor

It was from the ancient city of Merida that Capt Yancey made a number of flights to the capital of the Mayan Empire at Chichen Itza even landing in front of the famed Temple of the Serpents-the great Mayan pyramid The ability of Miss Champion to fly slowly and even hover over certain spots helped the archeologists make new discovshyeries that could have taken years on the ground Back in the United States subsequent flights into the Yosemite Valley in California and the crater of Crater Lake Oregon were a piece of cake by comparison

Miss Champion was not just a curiosity of her era Wherever she flew she engendered confidence in

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

And the rest is history

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VINTAGE AIRPLANE 37

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3 8 NOVEMBER 2009

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 17: VA-Vol-37-No-11-Nov-2009

Champion Spark Plug PCA-2 Pitcairn Autogiro undergoing rotor run-up tests at the factory-1931

An interested audience poses with Miss Champion at the Temple ofTigers Yushycatan February 1932

Company pilot Lew Yancey operates Miss Champion out of a clearing in the jungle of Mexicos Yucatan Peninsula This is the Temple of the Soldiers at Chichen Itza one of the Mayan ruins then being reclaimed from the rain forest At that time (1932) it was 100 miles from the nearest civilization

the method of flight as a truly safe form of aerial navigation She was a hard worker too often towing advertising banners over the cities she visited attracting valuable atshytention to the products her banner proclaimed The Champion comshypany declared in a letter to Pitcairn Aircraft the builder of its Autogiro that the value of the aircraft in inshycreasing sales and goodwill toward its products was beyond estimate

Miss Champion was one of the first of her type to appear in the United States and was retired from active service after setting a new altitude record on September 25 1932 of 21500 feet the highest a rotary-wing aircraft had ever flown In her way Miss Champion had been a missionary her clumsy apshypearance appealing to the imagishynation of the public and winning its confidence through her ability to deliver the goods with complete safety She was retired with honor as a permanent exhibit of Chicagos Rosenwald Museum of Science and Industry in the spring of 1935

After World War II the museum had to give up Miss Champion in fashyvor of more timely exhibits from the recent world conflict and this vintage lady was released into the knowledgeable care of AK Miller of Montclair New Jersey who kept her in his own museum for many years until he was forced to close it down and move to other quarters Miller couldnt bear the thought of giving up this magnificent relic of the pioneering era in American avishyation so he disassembled her and moved her into a barn on his farm in Vermont where she gathered dust for many years

Meanwhile Stephen Pitcairn (EAA 109260 VAA 4080) son of Harold Pitcairn the aviation pishyoneer and winner of the Collier Trophy for his development of the Autogiro in this country had begun the formidable task of colshylecting and restoring examples of his fathers aircraft The first to be completed by Steve was the PA-5 Mailwing originally built for his

VINTAGE AIRPLANE 19

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

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and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 18: VA-Vol-37-No-11-Nov-2009

father in 1928 Next was a PA-7 Sport Mailwing which won for Steve the Silver Age Champion Award at the 1983 EAA convention at Oshkosh Wisconsin

Somewhere along the line Steve heard about the autogiro owned by AK Miller After several attempts to communicate by mail Steve went to Vermont to visit Miller who was then in his 70s and fishynally succeeded in negotiating for the PCA-2 Autogiro NCl1609 some five years later Steve had it trucked to his hangar at the Trenshyton-Robbinsville Airport New Jershysey where the restoration process began in October 1982

Fortunately at this time George Townson (EAA 251901 VAA 9519) of Delran New Jersey a former Autogiro pilot and mechanic was available for a full-time commitshyment Georges impressive creshydentials include airframe and powerplant certificate with an inshyspection authorization and ground instructor certificate with most ratshyings He holds a commercial fixedshywing ticket and helicopter and Autogiro ratings along with flight instruction ratings for these types He is an accomplished practical 20 NOVEMBER 2009

engineer He is a member of the Society of Experimental Test Pilots making first flights in several exshyperimental rotorcraft in the 1940s including the worlds largest (Pishyasecki XHRP-1 tandem rotor) heshylicopter He built from scratch a small racing plane and a light tanshydem rotor helicopter

Before joining Stephen Pitcairn he had been chief inspector and director of engineering for a reshygional air carrier Under his supershyvision Miss Champion was stripped of her original cover (the logos and numerals were saved to be copshyied) and the painstaking process of inspection began Careful notashytion of items to be worked on were listed in order of priority Eightyshyfive percent of the original parts were refurbished and reinstalled but a few items had to be remanushyfactured since replacement parts did not exist Fortunately the origishynal Pitcairn factory drawings were in Steves possession

One of the most important tasks in the restoration process was the rebuilding of the rotor blades Each main spar had to undergo rigid Xshyray inspection to make sure there was no corrosion or cracks in the

steel tubes that served as the backshybone of these rotating wings Then each rib with its spar-attachment collar had to be inspected and very often replaced because of damage cracks or other defects

It was during this tedious but crucial part of the job that George noticed that the airfoil middotcurve of the ribs actually used in the rotor blades was slightly different from the curve called for by the Pitcairn engineering specifications Accordshying to this official document the airfoil used was the Goettingen 429 But when George placed one of the ribs he had removed over the official drawing he saw imshymediately that the curve was just slightly different

Methodically he checked each rib throughout the length of the spar but found the same small but definite difference Had someone made them all wrong or was this a planned departure from the origishynal specs Knowing the care with which the Pitcairn people did their jobs he reasoned that it was more likely that this was a deliberate deshysign modification He reached for the phone and called Carl Gunshyther the Pitcairn archivist and afshy

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

II have been flying now for over 25 years I am a Certified

Flight Instructor and let me tell you - not only is the personal

hometown family feeling of dealing with AUA wonderful year

after year they find a way to insure my precious airplanes at a

value bar none lower than any other companyI

- Charles Tippet

Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

AUA is Vintage Aircraft Association approved To become a member of VAA call 800middot843middot3612

Aviation insurance with the EAA Vintage Program oHers

Lower premiums with payment options - Additional coverages - Flexibility on the use of your aircraft - Experienced agents Owine quote request available - AUA is licensed in all states

Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 19: VA-Vol-37-No-11-Nov-2009

ter briefly outlining the problem asked him if he knew of anything in the old Autogiro company reshycords that would confirm or deny his suspicions

Requests of this kind were not new to Gunther who had presided over the records for more than 15 years As a matter of fact he had just recently set aside several engineershying reports that he thought might be helpful to Steve Pitcairn and his able restoration chief and in one of them he recalled seeing some stateshyments made by Paul Stanley one of the Autogiro companys key engishyneers about the design of the rotor blades used in the PCA-2 Autogiros

Within a few days George was holding in his hands the docushyments that confirmed his belief that this was a deliberate design modification The new airfoil proved on testing to be smoother and more efficient under flight conditions but the changes comshying on top of so many others as the Pitcairn team pioneered its way to new horizons of knowledge rated only a single sentence reference in the official engineering report That sentence however enabled George to properly rebuild the four rotor blades that allowed this unshyusual old bird to fly

Airfoils critical as they were proved to be only one of the facshy

tors necessary to the solution of the rotor problem Each blade had to be accurately weighed and their weights brought to within 2 ounces of each other and at the same time the spanwise center of gravity of all blades had to be kept within 18 inch of each other Inshyattention to these details could cause at least an uncomfortable ride from vibrations

Finally in the spring of 1985 Miss Champion was rolled out of the hangar to check her engine and rotor system As Steve Pitshycairn climbed into the cockpit to begin this initial testing proshycedure George Townson looked on somewhat apprehensively Steve activated the starter for the nine-cylinder J-6 Wright engine The ground-adjustable Hamilton Standard propeller swung jerkshyily a couple of times and as the engine rumbled into a throaty roar spun into a full shiny disc of whirling blades blowing swirls of dust behind the Autogiros upshyturned elevators

Satisfied that all was well so far Steve looked over at George who gave a little shrug of his shoulders and made a whirling sign with his forefinger Steve reached for the rotor clutch knob and pulled it firmly toward him to its lock posishytion Slowly the four large overhead

blades began their counterclockshywise spin Gradually Steve eased open the throttle and the rotor inshycreased the speed of its rotation

Soon the blades were standing straight out at right angles to the hub Both men were looking for signs of increasing vibration that would indicate some problem with the rotor George noticed that one of the blades seemed to be trackshying a bit lower than the others so he gave Steve the sign to cut power to the engine As it slowed to idling speed and the rotor gradually slowed down George walked over and told Steve to shut her down so he could check the blade settings

It was while this checking was going on that a small wrench beshying used to adjust one of the blades near its root fell and punctured a hole in the fabric on the wing beshylow Now a small wrench is not a heavy object and both men thought it strange that a puncture would result from this trivial event George went to his toolbox and brought back a Maule fabric tester Testing the area near the puncture he found it below allowable tolershyance He then tested other areas on the fabric-covered aircraft With only slight variations the result was the same The brand new fabric covering was definitely weak and would have to be replaced What a disappointment because it meant among other things that the Aushytogiro would miss EAA Oshkosh 1985 just one month away

Although the fabric tested low Steve and George decided to make three short test flights to 700 feet to check the systems rotor rpm in flight and control response etc These short flights the first in 51 years for Miss Champion proved the excellence of the original design and the painstaking care George gave to the restoration All systems worked above expectations

To determine the cause of the fabric deterioration samples were sent to a testing laboratory along with a description of what had happened When the report came

VINTAGE AIRPLANE 21

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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Charles Tippett Warrenton VA

bull Pilot for over 25 years

bull Certified flight instructor

bull Chuck Tippett Wing Walker at The Flying Circus Aerodrome

AUA is Vintage Aircraft Association approved To become a member of VAA call 800middot843middot3612

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

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Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 20: VA-Vol-37-No-11-Nov-2009

back it indicated the particular nishytrate dope formulation had an exshycess acid condition that resulted in the serious weakening of the Grade A cotton fabric The process of reshycovering and painting Miss Chamshypion with a new covering system was started in September 1985

Off to Oshkosh 86 Steve would not be denied flyshy

ing his rare Pitcairn Autogiro to Oshkosh 86 however the trip wasnt certain until the last minshyute Having only a total of four hours on the plane he departed on Thursday July 31 hoping to arshyrive at Oshkosh August I opening day of the EAA convention

He battled inclement weather associated with a warm front until crossing the Allegheny Mountains when things began to clear up

The first leg of his flight was one hour 45 minutes to a refueling stop at Carlisle Pennsylvania where he would also check his calculated fuel consumption There he landed into the wind across the runway utilizshying the short takeoff and landing characteristics of the Autogiro Alshythough the plane carries 52 gallons of fuel Steve planned his crossshy

22 NOVEMBER 2009

country legs at a conservative maxshyimum of 2 hours 15 minutes

His next stop was Beaver County Airport northwest of Pittsburgh and from there he flew to Bluffton Ohio (between Lima and Findlay) Unbeknownst to Steve at the time a nut had loosened allowing the oleo strut on the left landing gear to separate The wheel and its vee axle were dangling from the Nshystrut and although Steve was talkshying on UNICOM with the folks at Bluffton they didnt recognize the problem as they had never seen an Autogiro before

The touchdown on the runshyway was on the side of the ershyrant left wheel at an estimated 8 mph groundspeed The plane pivshyoted to the left going down on the left wing but fortunately not far enough to ding the groundshyadjustable Hamilton Standard propeller Due to centrifugal force holding them out the rotor blades didnt contact the runway until they slowed and were susshypended by their respective droop cables Only the rotor blade tips touched very lightly doing minishymal damage

The airport owner and manager

Harold Carey came out on his golf cart sized up the situation and said hed call the wrecker from town to hoist the plane and move it off the runway This was accomplished and it was moved into a hangar where it rested on some barrels while the landing gear was repaired

Steve contacted George Townshyson back home and he came to Bluffton to supervise the repair job Thanks to the assistance of some local folks and the availability of a machine shop and welding facilishyties the repairs were completed In the meantime Steves good friends Wayne Hays and his wife of Robshybinsville New Jersey left three days early on their vacation and brought to Bluffton the needed materials from Steves hangar including covshyering material paint and an extra set of streamline wires that had to be replaced between the two landshying gear N-struts

Wayne worked all the next day (Saturday) patching and painting the wing and rotor blades and by that evening Miss Champion was ready for a test flight Everyshything checked out okay and Steve departed on Sunday morning for Oshkosh

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 21: VA-Vol-37-No-11-Nov-2009

A refueling stop was made at Valparaiso Indishyana then on to Chicago where Steve flew along the lakeshore with a breathtakshying view looking up at the city s skyscrapers A final fuel stop was made at Hartshyford Wisconsin and at 130 on Sunday afternoon Aushygust 3 he touched down at Wittman Airfield-Oshkosh at last Time en route was 105 hours

Steve thrilled Oshkosh 86 convention-goers with his demonstration flights on Monday during the Pashyrade of Flight and again on Wednesday in the aircraft showcase preceding the air show The short-field takeoff and landing capashybilities of this 55 -year-old aircraft were most impresshysive as were the extremely short radius turns while airborne

It was interesting to watch the startup taxi and takeoff procedure for the Autogiro Taxiing is mostly conventional even without a steershyable tail wheel (it still has its origishynal skid) Steering on the ground is strictly by use of brakes a techshynique made somewhat easier beshycause of the wide (13 foot 3 inch) tread of the landing gear

Prior to takeoff the rotor blades are started into rotation by the pishylot pulling a knob in the cockpit that engages a clutch gearbox and shaft driven by the Wright J-6-9 A separate tachometer indicates the rotor speed and when 120 rpm is reached the rotor drive unit is disshyengaged full power is applied to the Wright and the pilot takes off No-wind takeoff distance is 250 feet maximum however under certain conditions its possible to make a jump takeoff with zero ground roll

Normal landing approaches are made at 20-25 mph forward speed but it is possible to slow the Autoshygiro in the air to zero forward speed and permit it to descend vertically

Listed here are specifications and performance data

Wingspan 30 feet

Length 23 feet 1 inch

Height 13 feet

Rotor diameter 45 feet

Rotor blade chord 22 inches

Empty weight 2233 pounds

Gross weight 3000 pounds

Maximum speed 119 mph

Cruising speed 98 mph

Landing speed Omph

Rate of climb 800fpm

Service ceiling 15000 feet

Gas capacity 52 gallons

Oil capacity 65 gallons

Cruising range 290 miles

Price (fly-away factory) $15000

to a landing In a Champion comshypany press release the vertical deshyscent speed was described as 14 feet per second slower than a parashychute The beautifully restored Pitcairn Autogiro would most cershytainly have received an award at Oshkosh 86 but Steve chose to not register it for judging

After Steves uneventful 95-hour flight home from Oshkosh in Miss Champion he began to do some things that time did not permit earshylier The plane was a little out of rig and that needed to be corrected The pitch of the Hamilton Standard propeller was set too low yielding a cruise speed of only 80 mph instead of the 95-98 called for in the specs

Autogiro rotor blades flap (modshyerately) up and down each pivoting on a pin in a bronze bushing and by the time he got home the bushings

Bibliography

were badly worn It was detershymined that the pins were not getting enough grease and posshysibly the bushings were made from the wrong material

New flying wires were orshydered for the rotor blades and the previously damaged landshying gear was taken apart to have new pieces made to reshyplace those which had been temporarily repaired on the flight to Oshkosh Not long after its return to New Jersey the landing gear was more neatly repaired

Epilogue Miss Champion continued to be the jewel in Steve Pitcairn s collection for more than two decades until he deshycided to donate the historic Aushytogiro to EAAs collection It is displayed at various times in both the EAA AirVenture Mushyseum and EAAs Pioneer Airport

Pitcairn Hangar Along with the Pitshycairn PA-18 restored by Leading Edge Restorations and the Pitcairn PA -39 donated earlier by Steve Pitcairn it was a featured attraction during this past years Good aI Days at Pioneer Airport-HG Frautschy

About the PCA-2 Pitcairn Aircraft built 20 or more

Model PCA-2 Autogiros in its plant on Pitcairn Field Willow Grove Pennshysylvania These three-place utility airshycraft quickly became promotional tools for various well-known comshypanies including the Detroit News newspaper Champion Spark Plug Company Standard Oil of New York Sealed Power Piston Ring Company Beech-Nut Packing Company and others The Detroit News Autogiro is on display at the Henry Ford Museum in Dearborn Michigan ~

1 Aircraft Biography Miss Champion by Carl R Gunther 2 Interview with Stephen Pitca irn 3 US Civil Aircraft Vol 5 by Joseph P Juptner 4 Pitcairn Aircraft Company brochure 5 Champion Spark Plug Company press releases and brochure

VINTAGE AIRPLA NE 23

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

Performing at The Flying Circus Aerodrome in Bealton VA

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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40 NOVEMBER 2009

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Page 22: VA-Vol-37-No-11-Nov-2009

BY ROBERT G LOCK

Materials ampProcesses Part 2

In the last issue we looked in detail at structural and nonstructural metallic components of older aircraft Now lets look at other materials and proshycesses that will be helpful in restoring and mainshy

taining our vintage aircraft

Control Cable Aircraft quality control cable is available in sizes from 116 to 38 inch in diameter For most vintage airplanes the maxishymum diameter used is 532 inch Two types of material are used to manufacture cable-stainless steel and carbon steel (which is coated with pure tin or zinc for corrosion protection) Either flexshyible or nonflexible type cable may have been used on the original airplane I suggest you use the type of cable originally installed however I have substituted corshyrosion-resistant cable for carbon steel especially where cables are subjected to the elements and corrosion is a problem

Incidentally researching the history of cable invention and production is very interesting On this subject one persons name comes to the forefront-John Roebling one of the pio-

When I attended

Northrop Institute of

Technology back in

1960-1961 to train for

my AampP we were

required to fabricate a

five-tuck cable to length

in FAA AC 4313-1B Section 8 Cable strength data will not be presented here After fabrication control cables are tested to a proof load which is a pull test to 60 percent of rated cable strength for three minutes

Cable assemblies are meshychanically fabricated the most common being swage-type tershyminals and the Nicopress proshycess The Nicopress-type cable ends may be used as a substitushytion for the Navy five-tuck woshyven ends used on most vintage aircraft The Nicopress process is most easily adapted for field manufacture of cables Swage cable end fittings require elaboshyrate squeezing tooling which is hard to find and very expensive Its interesting to note that the

neers of the wire rope industry Interesting reading can be found at the following websites

wwwInventionFactorycomhistoryRHAgenrstory rswarhtml

wwwglobalspeccomFeaturedProductsDetailLooshy5 WireDivSpecialty _wireJope_honors_legacy _of John_ Roebling401360

Flexible cables may have been used by the factory when the cable is not required to change direction

24 NOVEMBER 2009

drastically Flexible cable is designated as 7x7 It is composed of wire rope of six strands of seven wires each twisted and laid around a strand center or core consisting of seven wires

Extra-flexible cables are designated as 7x19 That is wire rope of six strands laid around the central core strand in a clockwise direction Each strand consists of 19 wires each Cable strength data can be found

newly revised AC 4313-1B manual has deleted both the wrapped and soldered and five-tuck woven cable ends However both these deleted methods appear in the terminated AC 4313-1A When I attended Northrop Institute of Technology back in 1960-1961 to train for my airframe and powerplant (AampP) certifishycate we were required to fabricate a five-tuck cable to length We made a cable clamp and marlin spike from scratch out of raw stock learning how to use hand

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

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DIRECTORS Steve Bender Jeannie Hill

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Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

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MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

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EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

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Page 23: VA-Vol-37-No-11-Nov-2009

tools and read blueprints I still have those tools to this day although they are a little rusted

Inspection of control cables should be made at the 100-hour and annual inspections Most cable wear takes place where the cables pass over a pulley or through a fair-lead To locate broken wire(s) in a strand run a rag along the cable In many cases the cable should be loosshyened so a close inspection can be made of the area that touches a pulley through full travel Bending the cable so that the portion that rubs on a pulley is on the outshyside of the bend will help reveal damage

Corrosion is another common type of damage It will show up on carbon steel cables as rust Replace any cable that shows signs of damage Again A C4313-1B is a good guide for cable inspection Figure 1 shows the method of detecting broken cable strands particularly where cable lays contact a pulley

Figure 1

Inspect pulleys for wear and ensure that pulleys roshytate when cable is moved

Always lube pulleys with a good lubricating oil Reshyplace any pulleys that show signs of wear or seizing of the bearing or bushing Sudden loss of cable tension can usually be traced to the cable wearing into a pulley

Inspect cable ends for wear or slippage Swage-type cable ends are painted red at the junction of the termishynal end and cable so slippage can be detected Again a sudden loss of cable tension should be investigated immediately Dont just retension the cable

Finally turnbuckles are used in a cable system to provide a means of tensioning They actually adjust the length of the cable Cable tension on vintage airshycraft is relatively small from 10 to 25 pounds The reashyson is the pulleys did not have a bearing in the center just a bronze bushing The more tension on a cable the heavier the control movement Adjust tension to give good control response and safety the turnbuckles

I have found that 10-20 pounds of tension is good for these type systems

When installing turnbuckles it is necessary to screw both threaded terminals into the turnbuckle barrel an equal amount It is essential that cable terminals be screwed into the barrel so that not more than three threads on the terminal are exposed Be sure to secure both cable terminal ends when screwing a turnbuckle dont allow cable to twist during this operation

There are two methods of safety wiring turnbuckshyles-single and double wrap The correct method for wrapping turnbuckles is shown in AC 4313-1B Figure 7-24 Pay close attention that the correct size safety wire be used when safetying cable terminals This is a most common area where mistakes are made AC 4313-1B gives appropriate wire type and diamshyeter for this process Either copper brass stainless steel monel or K monel may be used NOTE Oneshysixteenth-inch and 332-inch cables may be single wrapped only with copper brass or stainless steel safety wire at least 0040 inch in diameter For cables of lI8-inch diameter single-wrap safeties are made with 0040-inch stainless steel safety wire If a singleshywrap safety using copperbrass wire is desired the diameter must be 0057 inch Ive never used or seen 0057-inch brass wire However lI8-inch cables may be double wrapped and safetied with copperbrass or stainless steel wire UNDER NO CIRCUMSTANCES SHOULD 0032-INCH DIAMETER WIRE BE USED TO SAFETY ANY TURNBUCKLE It might be wise to do a turnbuckle safety wire check of your airplane Figure 2 shows both single- and doubleshywrap safety of turnbuckle

Only cable terminal ends and fittings that meet AN standards should be used in aircraft applications AC 4313-1B gives directions on how to properly safety a turnbuckle

And lastly cables tend to stretch after fabrication and it may be necessary to retension the cables after a few hours of flight When retensioning cables always make the same adjustment to cables that pull against each other In other words if the aileron system has three turnbuckles adjust all three the same amount of turns and the travel will not be affected only the tenshysion will increase

Tubing Aluminum tubing is commonly used to fabricate fuel oil hydraulic and instrument sysshytem installations Alloy 3003 is most easily bent and flared followed by 5052 and finally 6061 Since most vintage restorations require hand-forming and flarshying only these alloys should be considered In the softest state the code will be an 0 indicating the annealed condition An example would be 5052-0 Alloy 6061 would show a hardness code of -T6 (6061shyT6) indicating the tube has been heat-treated and arshytifiCially aged It is difficult to bend and flare this tube type but not impossible

VINTAGE AIRPLANE 25

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

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Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

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DIRECTORS Steve Bender Jeannie Hill

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DIRECTORS EMERITUS

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EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

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Page 24: VA-Vol-37-No-11-Nov-2009

(D) SINGLE WRAP

(B) DOUBLE WRAP

Figure 2

Tube Bending Alloy 3003-0 tube can be handshybent even small radius bends This tubing should be used for instrument installations where the pressure is low and tubing is protected Alloy 5052-0 tubing can be hand-bent but the bend radius must be large to prevent flattening or kinking of the tube in the bend radius Use of hand-bending tools is recommended Alloy 6061-T6 can only be bent with a hand-bending tool using a substantial bend radius Always check tube flattening in the bend radius for fuel lines the maxishymum flattening is 5 percent of tube diameter

Tube Flaring Aircraft tubing is flared to an angle of 37 degrees Do not use automotive flaring equipshyment as the flare angle is 45 degrees The older aircraft used AC fittings While the flare angle is the same AC fittings are not interchangeable with AN fittings Most modern restorations will convert fittings to AN due to ease of procurement Tubing should be flared so as much of the flared area of the tube as possible seats on the AN fitting Always check flared area for cracks parshyticularly alloy 6061-T6 tubes

Alignment of tube to fitting is also critical Misalignshyment will eventually cause leaks at the fitting

Tube Installations For instrument installashytions use 3003-0 tubing 1I8-inch (-2) or 316shyinch (-3) diameter Some restorers may want to use 5052-0 tube for oil the pressure gauge For fuel inshystallations use 5052-0 tubing most often Vz-inch (-8) diameter AC 43 13-1B gives much information on fuel systems particularly the location of support clamps and fuel line bonding information Consult Chapter 8 Section 2

I dont like using copper tube in aircraft applications because it will work-harden with vibration I know all early aircraft used it for fuel and instrument installashytions so if authenticity is the goal use it However copper tubing may need annealing from time to time Anneal by heating and quenching in oil (Editors note Remember Charles Lindberghs admonition to the people

building the Spirit of St Louis he required the interruption of the fuel lines with sections offlexible nlbber hose to soak up vibration and prevent breaks due to work-hardening of the tubing material-HG Frautschy)

Tube Fittings The most common tube fittings are the AN818 nut and AN819 sleeve Most aviation supply company catalogs give a list with description of all AN fittings needed to complete the project I keep a copy of the Standard Aircraft Handbook in my toolbox for quick reference of the AN code Since Im writing this in Florida a nearby source for this handy book is wwwGreat-Atlanticlcom Look for part number TS157642-8 Most suppliers carry this book youll find it very useful

Low-Pressure Oil System Dry sump oil systems use tubing of 1 inch in diameter The tube can be 5052shy0 and special tools are required to bend it to the deshysired shape After bending the tube is beaded on both ends using a beading tool Be sure to remove all burrs after beading and clean the tube before installation

Tube Installation After fabrication of necessary tubing be sure to clean thoroughly and blow-dry with compressed air Assemble with proper hose and clamp using stainless steel hose clamps The tube ends should never touch as this would allow fragments of alumishynum to enter the oil system Maximum distance beshytween tube ends is one tube diameter

Hose For fuel and oil systems use only Mil-H-6000 hose It will come in inside diameter sizes -4 (14 inch) through -112 (lVz inches) The burst pressure for this type hose is 1000 psi and it is resistant to fuel oil and coolants For pitotstatic instrument systems I have used rubber heater hose or Tygon B-44 type flexshyible plastic tube but not in antique restorations For fuel and oil systems I use stainless steel hose clamps Tighten clamps to torque of just 20 inch-pounds and dont over-tighten

Thats it from here Lets keep those antiques safe and flying

26 NOVEMBER 2009

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

for the Holidays Santa in Plane Ornament Wimsical metal ornament has Santa in the pilots seat Has adetachable metal spring that gives Santa an action ride of high and low altitudes

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Airplane Banks Shaped like their favorite airplane theyre perfect for the airplane themed bedroom Our banks are made from resin and are handpainted with abright glaze Measures approximately 7 by 7 by 4W Red Mustang $995 52648598 Heliocopter $995 2648597 Biplane $1295 V52652826

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 26: VA-Vol-37-No-11-Nov-2009

Light Plane Heritage PUBLISHED IN EAA Experimenter MARCH 1989

THE MUMMERT COOTIE

Immediately after World War I Harvey Mummert was one of the earliest designers and builders of homebuilt air shyplanes His several originalshy

design lightplanes were built in his spare time with the help of friends while he was employed as an engineer for the Curtiss comshypany at its Garden City Long Isshyland plant All his airplanes inshycorporated advanced features and showed skillful application of exshycellent design both aerodynamic and structural

Mummerts first lightplane apshypeared in 1921 after two years

BY JACK McRAE EAA 93

of work and was a very attracshytive miniature biplane called the Baby Vamp which soon came to be known as the Cootie The first flight of the Cootie was made on July 8 1921 by the well-known pilot Bert Acosta Some diffi shyculty was encountered before the flight when it was discovered that Acosta had to remove his shoes in order to get his feet through small holes in a bulkhead to operate the rudder bar

On the first flight the pilot reportedly held the ship on the ground for 200 feet before taking off When it got off the ground it

was seen to be flying very steadily and at a speed estimated to be nearly 100 mph Acosta who was noted for his fondness for aeroshybatics proceeded to put the little biplane through an Immelmann and many other maneuvers reaching 1500 feet altitude withshyout any difficulty After 15 minshyutes of flying he landed smoothly and reported that liThe machine has absolutely no tricks and needs very few minor adjustments

The engine used in the Cootie was reported to be a 25-hp Lawshyrance which would imply that it was a surplus Type A engine as

Editors Note The Light Plane Heritage series in EAAs Experimenter magazine often touched on aircraft and concepts related to vintage aircraft and their history Since many of our members have not had the opportunity to read this seshyries we plan on publishing those LPH articles that would be of interest to VAA members Enjoy-HGF

28 NOVEMBER 2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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40 NOVEMBER 2009

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Page 27: VA-Vol-37-No-11-Nov-2009

I JI ---I shy i-shy

I

I--4___- I

I

1 ~

k

Harvey Mummert and the Mummert Cootie

l 1I

HOWEVER CLOSE

EXAMINATION OF

THE COOTIE

PHOTOGRAPHS

INDICATE THAT THIS

WAS NOT THE CASE

AND THAT THE

ENGINE WAS THE

RELATIVELY RARE

LAWRANCE N MODEL

OF WHICH ONLY A

FEW WERE BUILT FOR

THE US NAVY

used in the Penguin ground trainshyers However close examination of the Cootie photographs indicate that this was not the case and that the engine was the relatively rare Lawrance N model of which only a few were built for the US Navy The Type N engine had the inshytake manifold at the front and the valve pushrods at the rear the opshyposite of that for the Type A used in the Penguin s The N engine also had advanced features such as dual ignition supplied by a batshytery dual carburetors and a gear drive to the propeller Its weight was only 79 pounds and its width was much smaller than the Type A Its displacement was 12058 cubic

1921 MUMMERT COOTIE

LAWRANCE ENGINEd~L~ I o ~ 3 4shyIf- I

SCALE IN FEETJ0

VINTAGE AIRPLANE 29

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

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race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

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VINTAGE AIRPLANE 39

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Page 28: VA-Vol-37-No-11-Nov-2009

The Mummert Cootie with a Burnelli RB-l airliner in background

The Cootie gets a thorough inspection at a Curtiss Field air show

The Main Characteristics of the Cootie Span 18 feet

Length 12 feet

Chord 31-58 inches

Gap 33 inches

Wing area 90 square feet

Weight empty 350 pounds

Gross weight 590 pounds

Maximum speed 100 mph

Landing speed 43 mph

Fuel capacity 12 gallons

Oil capacity 2 gallons

inches and it developed 40 hp at 1900 rpm although it was stated that the engine speed was limited to 1500 rpm during the flight test The N engine had one bad feature of the Type A however in that it still had the single-throw crankshyshaft which caused severe vibrashytion and in one case reportedly shook a carburetor off in flight It is assumed that Mummerts posishytion in the Curtiss engineering deshypartment gave him access to this unusual engine

At that time Curtiss had just started building its famous series of racers using wooden monoshycoque fuselage construction with plywood-covered wings The Cooshytie used these same features the fuselage being built of three layshyers of veneer strips at 45 degrees to each other wrapped around a wooden form and glued after which the form was removed and bulkheads installed where necesshysary The tail surfaces were also all wood including the covering

The wings which used th e RAF 15 airfoil were each built as a single unit with no dihedral Each wing used nine spars between the leading and trailing edges The spars were of rectangular section l4 -inch wide and varied in depth according to their chordwise loshycation The maximum thickness of the wing was only 2 inches The upper rear main spar and the lower front main spar were of the box type since they made up part of the wing truss and had to reshysist axial loads due to the flying and landing wires Mahogany plyshywood 116-inch thick was used to cover the wings This type of conshystruction gave a smooth streamshyline shape of great rigidity The inshyterplane struts were of streamline steel tubing and the upper wing was supported by two cantilever struts at the center of the wing The flying wires consisted of a pair of streamline wires on each side running from the fuselage at the lower front spar to the upper rear spar at the interplane strut

30 NOVEMBER 2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

Covers all major events of each race year Over 50 min of archival newsreel footage amp never-be fore-seen color film More than 600 rare photographs Narrated story describes all the exciting action in this 2 hrlO min DVD

1939NARDVD 90 min in-depth and complete reporting of the last pre-war

race Narrated story and hundreds of original photographs Over 45 min of outstanding rare color film shot at the races

~~9JCd

some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

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Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

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For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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40 NOVEMBER 2009

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Page 29: VA-Vol-37-No-11-Nov-2009

fitting The landing wires were a single wire on each side of the airshyplane running from the lower end of the front interplane strut to the top of the rear cabane strut

Apparently afte r flight testing two additional wires were added on each side extending from the rear upper and lower interplane stru t fi t t ings to the fi rewall bulkshyhead just aft of the engine The reason for these additional wires is not known but they may have been added in an attem pt to abshysorb some of the engine vibration or possi bly to red uce the effect of defl ection of the cantilever cashybane struts under unsym metrica l wing loads

Ailerons we re ins talled on the lower win gs only and extended for the full wing span Th e aileshyrons were controlled by a horn at the airplane centerline inside the fuselage with no external fitt ings

Th e fin of u p p er and lower sect ion s was built integral with the fu selage and the t a il skid was attached to its lower section Elevato r and rudder cables we re kep t i n side the fu se lage with their contro l horn s enclosed in the thickened fuselage section at the tail post

Th e lan ding gear was o f t he spreade r bar type wit h str eamshyline struts of ash and with shock cord attaching the axle Side loads were taken by diagon a l wi res in the plane of the rear landing gear struts an d anoth er pair of wi res extended to the firewall bulkhead

Th e Cootie was used for exhishybition flying at various air shows held at Curtiss Field for severa l yea rs and it was flown by such well-known pilots as Bert Acosta and Lloyd Bertaud Its fina l disposhysition is not known

References Aeria l Age July 25 1921 Flight Jan u ary 191922 Aerosphere 1939 Skyways April 1988 Interviews with Curtiss enshygineers of the 1920-30 era Photos are fro m the collection of Gabe Baumwart Curtiss engineer

Harvey Mummert

Harvey C Mummert Pilot Designer and Manufacturer Harvey C Mummert was born in Alliance Ohio

on April 4 1892 He graduated from Mount Union

College Alliance and the Case School of Applied

Science in Cleveland

In 1916 he started work for the Curtiss company

in Buffalo as an engineer and his signature appears

on some 1916 IN-4 drawings He apparently made

good as an engineer and in 1918 he was transferred

to the Curtiss Experimental Engineering plant in Garshy

den City Long Island Here he had responsible posishy

tions in the design and development of the MF Flyshy

ing Boat and the Eagle eight-passenger tri-motored

biplane in 1919 the twin-engined CJ NavalTorpedo

monoplane the PW-8 fighter and asmall all-metal

seaplane glider designed for the use of Glenn Curtiss

One of his co-workers describes Mummert as A very

mild mannered man with an unusually keen mind and asense of sound practical design

Since his days in high school he had been interested in small airplanes and in the 1921-24 period he

designed and built in his spare time three successfullightplanes These were the 1921 (ootie biplane

with aLawrance engine the 1923 midwing monoplane of wood monocoque construction using a

Harley-Davidson motorcycle engine and in 1924 an all-wood low-wing cantilever monoplane also

Harley-powered which competed in the 1924 and 1925 National Air RacesMummert was amember of

the Curtiss Flying Club atthis time and in 1924 he received Federation Aeronautique Internationale (FAil

Aviation PilotsLicense No6169 In 1927 he received Transport Pilot License No 550

In 1924 Mummert left Curtiss and became chief engineer for the newly reorganized Mercury Aircraft

Inc of Hammondsport New York During the next 15 years at the Mercury company Mummert was

responsible for anumber of interesting deSigns as follows

1924 - Mercury St Liberty-powered biplane awinner of Mail Plane competition held by the Post

Office Department

1925 - Redesigned Standard J-1 to five-seater C-6A-powered and as atwo-place trainer Five sold

to Argentine government

1925 - Mercury Jr two-place utility biplane C-6A engine Flown by Mummert in 1925 National Air

Races and in the 1925 1926 and 1927 Ford Airplane Reliability Tours placing third in 1927

1926 - TC-11 nonrigid training blimp delivered to Army in 1928

1927 - Mercury Kitten two-place cabin monoplane of all-steel tube construction Originally powered

by Mummert-designed two-cycle four-cylinder opposed-piston engine later with Warner Scarab

1929 - Schroeder Wentworth Safety Plane for Guggenheim Safety Competition Crashed during

qualifying flights

1929 - Mercury Chic T-2 primary trainer Approximately 20 built Flown by Mummert in Ford Nashy

tional Air Tours 1930 and 1931

1930 - Mercury S Racer Flown by Mummert in 1930 All -American Flying Derby a5540-mile race

1931 - Mercury S-1 Racer Steel tube geodetic construction Flown by Mummert in National Air

Races and other local air shows

1938 - Mercury Chic modified and entered in Air Corps Primary Trainer competition at Wright Field

In 1939 after ashort illness Mummert died at the age of 47 He had been aprolific innovative

designer with astrong competitive spirit as demonstrated by his many entries in air races and air tours

flying airplanes of his own design

References American Airman February and March 1961

VINTAGE AIRP L ANE 31

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

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Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

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Page 30: VA-Vol-37-No-11-Nov-2009

BY DOUG STEWART

All available info evant parts of FAR 91103 just for a moment lt states Each pilot in command shall before beginning a flight become familiar with all available information concerning that flight This information must include (a) For a flight not in the vicinity of an airport weather reshyports and forecasts fuel requireshyments alternatives available if the planned flight cannot be comshypleted (b) For any flight runshyway lengths at airports of intended use

Lets take a look at where we might go to obtain all that availshyable information and as well how to document that we have indeed gotten all that informashytion Let us also be aware that the terms all available information II

and in the vicinity of an airport are not defined in FAR Part 1 Thus there is the potential to incur a vishyolation of these regulations predishycated upon the interpretation of a local FAA inspector Whether their interpretation stands up would remain to be determined by the National Transportation Safety Board but in the meantime if a pilot is charged with a violation that pilot would have to spend significant time and expense in his or her own defense

Certainly one of the best places to start is either with a briefer or by obtaining a direct user access terminal system (DUATS) briefshying Regardless of which source we use there is a record kept of our having gotten that briefing I

As I was departing the patshytern of my home base airport a few days ago heading out to the pracshy

tice area to do some air work with a client in my PA-12 I overheard a pilot announce that he was 10 miles out to the southwest and inshybound for landing Hearing that I knew that I would have to be esshypecially diligent in my see and avoid collision avoidance scan as I was headed to the south myself

But the next thing the pilot said increased my concern He asked Uh which runway you using at Columbia County Since I had just announced not only the runway I was departing on but further the direction of my deparshyture and since there were several other planes in the pattern all making proper announcements of what they were doing I couldnt help but wonder if this inbound pilot was using his ears as well as his mouth

As the communications conshytinued my concern increased His next communication asked which way the wind was blowing As there is an automated weather observing system (AWOS) at the airport it was obvious that this inbound pilot had not spent the time listening to it to find out all the pertinent information relative to the ceiling visibility wind and barometric pressure At this point I decided to alter my course to the southeast and increase my vigishylance out the window

32 NOVEMBER 2009

Within a minute or two the inshybound pilot now asked Uh Columbia County Uh do you have right- or left-hand trafshyfic At this point the hackles went up on the back of my neck What was up with this inbound pilot

Had he done

no planning

whatsoever for

his flight

Had he done no planning whatsoshyever for his fl ight Was he totally reliant upon others to give him the information that he needed Did he not have a sectional chart or an AirportFacility Directory (AFD) with him in the airplane that provided at least some of the information for which he seemed ignorant Im surshyprised he didnt ask the traffic patshytern altitude as his next question And lastly was he unaware of FAR 91103 Preflight Action

Lets review some important relshy

cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

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VINTAGE AIRPLANE 37

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spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

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VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

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cant help but wonder it the pilot described above had bothered to get a briefing Had he come to the airport yesterday at the same time of day as he had in the described scenario he would have had a chance to observe some military aircraft up close and personal as our airport was closed for a presishydential temporary flight restricshytion (TFR) until late afternoon Nowhere in 91103 do we see TFRs included in all available informashytion I but I can assure you that this regulation would be referred to in the document charging a pishylot with a violation

There are certainly many other resources for obtaining weather information in addition to flight service and the DUATS prOViders and many of us myself included do indeed use those resources In fact I typically look at several difshyferent Internet websites to obtain some fantastic weather informashytion AviationWeathergov headshying the list For me a picture is worth a thousand words and the graphical information available on these websites makes my selfshybriefing much more valuable But the question remains how do we document that we have been to those websites The simplest way I know is to print out the relative web pages we have viewed

It might be difficult to prove that we have ensured sufficient fuel for the trip and I can assure you that many pilots have been successfully charged with violation of 91103 in fuel exhaustion accidents and incidents Quite often these violashytions come about as a result of the pilots own admission of negligence in one way or another Forewarned should be forearmed

Okay you say that your flight will be in the vicinity of the airport and therefore you might not have gotten a briefing But let us all be aware that the FAA chief counsel said that The FAA has no specific fixed definition of vicinity but instead interprets its meaning on a case-by-case basisI (1-28-92) In

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some situations anything away from the traffic pattern might be interpreted as not in the vicinity of the airport All I will say here is that a word to the wise should suffice

Let s go back to that pilot inshybound to my home base On that particular day the wind had been lightly blowing out of the south all day long Had our errant pilot gotten a briefing he should have been aware of that fact even if he was oblivious to the tail wind pushing him northward With the runway at my home base aligned 03-21 it should have been self-evshyident that landings that day would be to the south

But even if he hadnt been aware of the southerly winds a check of the AWOS prior to reaching 10 miles out would have informed him of the winds Certainly if he had a current sectional on board that frequency would have been available to him And the quesshytion about right- or left-hand trafshyfic would have been answered on that sectional as well If there were right-hand traffic for either or all runways it would be denoted in the airport data information on the sectional chart with the notashytion RP and for which runway(s)

Another source for this inforshymation is the AirportFacility Direcshytory also known as the little green book Perhaps you live in an area where it is difficult to get a curshyrent copy of the AFD And it will be getting even harder as the govshyernment cuts back on the number

of fixed base operators and flight schools that can sell these as the government increases the volume requirements to qualify as a dealer If that is your situation please be aware that the AFD is now availshyable in a digital format on the FAA website Go to wwwNACOFAA govindexaspxml=nacnlined_ afd where you can download the information for the airports of your intended landings

There are some pilots who would consider the term all available inshyformation as somewhat ambigushyous and therefore disregard the need to get as much info as they can prior to a flight Failing to do so might get a pilot in trouble with the FAA but more importantly not having as much information as one can possibly have could put one in an unsafe situation A pilot who just kicks the tires and lights the fires without finding out as much as possible about everything relative to the flight is being neglishygent in the duties of being a pilot in command

So the next time you are beckshyoned aloft by blue skies and tail winds be sure that you launch with as muchavailable informashytion as you can get

Doug Stewart is the 2004 National Certificated Flight Instructor of the Year a NAFI Master Instructor and a designated pilot examiner He opershyates DSFI Inc (wwwDSFlightcom) based at the Columbia County Airshyport (lBl) ~

VINTAGE AIRPLANE 33

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

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VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

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Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

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VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

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DIRECTORS Steve Bender Jeannie Hill

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40 NOVEMBER 2009

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Page 32: VA-Vol-37-No-11-Nov-2009

BY HG FRAUTSCHY

THIS MONTHS MYSTERY PLANE COMES TO US FROM WES SMITH

Send your answer to EAA Vintage Airplane PO Box 3086 Oshkosh WI 54903-3086 Your answer needs to be in no later than December 20 for inclusion

Be sure to include your name plus your city and state in the body of your note and put (Month) Mystery Plane in the subject line

in the February 2010 issue of Vintage Airplane

You can also send your reshysponse via e-mail Send your answer to mysteryplaneeaaorg

AUGUSTS MYSTERY ANSWER

O ur August Mystery Aviation (Lane DR The Thaden Corps pilot (1) and aeronautical Plane came to us from Argonaut All Metal Six Passenshy engineer Herbert von Thaden the EAA archives Wes ger High Wing Cabin Monoplane While Thadens wife Louise Smith did the follow- Is Powered With a Pratt amp Whitney is much better-known in aviashy

ing extensive write-up for us Wasp Engine February 13 1928 tion circles due to her extensive pp 386-388) the T-1 was the record-setting flying skills and

Descri bed in the pages of brainchild of ex-US Army Signal contributions to numerous aviashy

34 NOVEMBER 2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

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VINTAGE AIRPLANE 37

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In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

Something to buysell or trade

Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

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VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

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DIRECTORS Steve Bender Jeannie Hill

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Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

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chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

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bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 33: VA-Vol-37-No-11-Nov-2009

tion organizations Herbert von Thaden designed at least three aircraft between 1928 and 1930

Constructed at San Francisco by the Thaden Metal Aircraft Co the T-1 (NX3902) was test-flown at Crissy Field The steel framework was covered with corrugated dushyralumin which is alleged to have given the airplane better-thanshyexpected performance Patented removable panels (Thaden held four US aeronautical patents) on the underside of the wings alshylowed relatively easy and thorshyough inspection of the underlyshying structure and fuel tanks The box wing spars were covered with the same corrugated duralumin as the skin and were permanently riveted to the upper surface The fuselage utilized Thadens unique monocoque construction that employed transverse members combined with stressed corrushygated skin in place of longerons Bulkheads in the cabin and tubushylar duralumin frames were used aft of the cabin but no longitushydinal members were used aft of the engine mount The fuel tanks (120 gallons enough for a sixshyhour duration) were mounted in the wings above the access panshyels and the fuel was fed directly into the carburetor with no fuel line entering the cabin A fireshyproof bulkhead separated the enshygine from the cabin for extra proshytection against fire

The undercarriage was of a split oleo-pneumatic type with hinged tripod strut-work Each half of the main gear also incorporated a Gruss shock absorber and the stout-looking tailskid incorposhyrated a pneumatic shock absorber Sauzedde wheels and brakes were fitted to the main gear

The strut-braced wings had a span of 53 feet 8 inches the fuseshylage a length of 35 feet 3 inches and the height was 11 feet which gave the Argonaut an imposing physical appearance The cabin normally seated six passengers but could be arranged to accomshy

modate up to eight persons The control surfaces and stabilizers were of the same construction as the rest of the airframe The conshytrols were operated by pushrods and a control yoke suspended from the engine mount was used for longitudinal and lateral conshytrol Conventional rudder pedshyals operated the rudder A wheel located to the right of the pilots seat was used to operate the elshyevator trim and the horizontal stabilizer was ground-adjustable The passenger cabin of the T-l

THE STRUT-BRACED

WI NGS HAD A SPAN

OF 53 FEET 8 INCH ES

THE FUSELAGE A

LENGTH OF 35 FEET

3 INCHES AND THE

HEIGHT WAS 11 FEET WH ICH GAVE

TH E ARGONAUT AN

IMPOSING PHYSICAL

APPEARANCE

was insulated and soundproofed for passenger comfort and a heatshying and ventilation system was inshycorporated The seats were made of wicker and ample legroom was provided An oval entrance door located on the left side of the cabin allowed ingress into and egress from the cabin A unique aspect of the door was that the corrugations did not run perpenshydicular to the frame being angled instead A baggage compartment was located just aft of the cabin and windows made of shattershyproof glass gave the passengers a good view of the outside

Empty weight of the aircraft was 2900 pounds and a useshyful load of 2200 pounds could be carried The 415-hp Pratt amp Whitney Wasp was originally deshysigned as the competitor to the Wright Simoon The first engine

was ready by Christmas of 1925 and after testing in the Wright F3W-l Apache it was placed into production in late 1926 By early 1927 12 were being delivshyered per month The engine actushyally displaced 1344 cubic inches (rounded off to 1340 cubic inches for statistical purposes) and had a bore and stroke of 575 inches The T-1 used a Wasp A of 400-420 hp and a ground-adjustable Stanshydard propeller First flown on 15 January 1929 the T-l was found to have a maximum speed of 135 mph a cruise of 105 mph and a minimum speed of 52 mph

Thaden drew his engineering force from Handley-Page in Engshyland from Ford in Detroit and from top American technical schools ET Todd associate engishyneer at the Thaden Metal Aircraft Corp was like his peers required to have actual aviation experience as a pilot a unique aspect of the company Organized at San Franshycisco RE Fisher was company preSident with Donald McKee as secretary WD Dickey as treashysurer WA Bechtel as chairman of the executive committee and EH Heller and CAA McGee as counsel Thaden served as vice president and manager

Following the 1928 T-l the T-2 (7074 cln 2) was also constructed in 1928 Described in Flight (The Thaden T-2 An American All Metal Commercial Monoplane January 10 1929 P 26) it was broadly similar to the Argonaut but was smaller Powered by a 150-hp Comet it had a span of 39 feet and an overall length of 26 feet Unlike the T-l the four-place T-2 had a fully cantilevered wing with trailing edge flaps The T-2 had a VMAX of 121 mph aVe of 90 mph and a VM1N of 46 mph The useful load was 1180 pounds

The T-3 was apparently never built but may have been modified to become Thadens last airplane the T-4 Constructed in 1930 as a Group 2 certificated aircraft (2shy247) the T-4 was powered by a

VINTAGE AIRPLANE 35

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Te lephone Or ders 800middot843middot3612 From US and Canada All Others Call 920middot426middot59121 Or sendto EAA Mail Orde rsPO Box3086 Oshkosh WI 54903-3086

Lim ited suppli es available middotShipping and handling NOT included Major credit cards accepted WI residents add 5 sales tax

Airplane Banks Shaped like their favorite airplane theyre perfect for the airplane themed bedroom Our banks are made from resin and are handpainted with abright glaze Measures approximately 7 by 7 by 4W Red Mustang $995 52648598 Heliocopter $995 2648597 Biplane $1295 V52652826

Wooden Planes Durable unpainted wooden planes are great for childs play Approximate size is

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Airplane Picture Frame Ideal for the nursery or youngsters room decor to display your favorite 4 x 6 photo of the young aviator The picture frame is hand glazed resin and measures about 8 W by 6 34with 3-dimensional clouds and airplanes 52652824

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Mini Maglitereg Rugged aluminum conshystructed flashlight with

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300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

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Friendliest manual around pofyfibercomToll-free technical support information polyfibercom Aircraft CoaUng_80Cgt-361-3490

VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

Something to buysell or trade

Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

MISCELLANEOUS Flying wires available 1994 pricing Visit wwwf1yingwires

com or call 800-517-9278

wwwAeroListorg - Aviations Leading Marketplace

SERVICES Always Flying Aircraft Restoration LLC Annual

Inspections Airframe recovering fabric repairs and complete restorations

Wayne A Forshey AampP amp LA 740-472-1481 Ohio and bordering states

TAiUAlt-66LS

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Vintage Tires New USA Production

Show off your pride and joy with a fresh set of Vintage Rubber These newly minted tires are FAA-TSOd and speed rated to 120 MPH Some things are better left the way they

were and in the 40s and 50s these tires were perfectly in tune to the exciting times in aviation

Not only do these tires set your vintage plane apart from the rest but also look exceptional on all General Aviation aircraft Deep 832nd tread depth offers above average tread life and UV treated rubber resists aging

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continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

152 1 E MacGregor Dr N57W34837 New Haven IN 46774 Oconomowoc W I 53066

260-493-4724 262-560-1949 cl1ief7025(gaoicol1l gdallbueramp-eaaorg

Secretary Treasurer Steve Nesse Charles W Har ris

2009 Highland Ave 72 15 Eas t 46th St Albert Lea M N 56007 Tulsa OK 74 147

507-373- 1674 9 18-622-8400 s171es2009ivtC0111 (whhvsucom

DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

David Bennett Espie Butch Joyce 375 Killdeer Ct 704 N Regional Rd

Li nco ln CA 95648 Green sboro NC 27409 9 16-645-8370 336-668-3650

anl iq llcrinreacl1com wdsockaucom

Jerry Brown Dan Knutson 4605 Hickory Wood Row 106 Tena Marie Circle

Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

Ibrow14906aol coln odicl lbclmrter llet

Dave Clark Steve Krog 635 Vesta l Lane 1002 Heather Ln

Plainfield IN 46 168 Hartford W I 53027 3 17-839-4500 262-966-7627

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Northborough MA 0 1532 Brookfield W I 53005 508-393-4775 262-782-2633

copeland IjIll ICJ(UnI Ill lperexecpccOl

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Lawton M I 49065 Wauwatosa W I 532 13 269-624-6490 41 4-77 1- 1545

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Dale A Gustafson 7724 Shady Hills Dr

Indian apoli s IN 46278 3 17-293-4430

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DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

Chicago IL 60643 Union IL 60180 773-779-2105 8 15-923-159 1

pllOtopiotaolcom bllck7acsmail com

Ge ne Chase Gene Morris 2 1 S9 Carlton Rd 5936 Steve Court

Oshkosh WI 54904 Roanoke TX 76262 920-23 1-5002 817-49 1-9 110

GRCH ACkllar t er 1let selenlOrrisCw rter l1et

Ro nald C Fri tz 1540 I Sparta Ave

Kent Ci ty M I 49330 616-678-50 12

EAA and Division Membership Services (800 AM-700 PM Monday-Friday CST) 800-564-6322 FAX 92042amp4873 www_ eaaorgjmemberbenefits membershipeaaorg

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EAA AirVenture Oshkosh 888-322-4636 wwwairventure_org airventureeaaorg Sport PilotLight-Sport Aircraft Hotline 877-359-1232 wwwsportpilotorg sportpiloteaaorg

Programs and Activities Auto Fuel STCs 92042amp4843 dwalkereaaor

Education Aeroscholars 920-426-6570 mrobbinseaaorg bull EAA Air Academy 920426-6880 www_airacademy_org airacademyeaa_org bull EAA Scholarships 920426-6823 scholarshipseaaorg

Rigilt Instructor information 920426-6801 www_eaaorgjnafi tdeimereaaorg Library Services Research 92042amp4848 slurveyeaaorg

Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

EAA Enterprise Rentshy A-Car Program 877-421-3722 www_eaa_orp)enterprise membershipeaaor~

Editorial 920-426-4825 www_ vinta~eaircraft_ or~ vinta~eeaaor~

VAA Office FAX 920426-6579 tbookseaa_org

EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 34: VA-Vol-37-No-11-Nov-2009

for the Holidays Santa in Plane Ornament Wimsical metal ornament has Santa in the pilots seat Has adetachable metal spring that gives Santa an action ride of high and low altitudes

52648599 $1295 Order Online wwwvintageaircraftorg

Te lephone Or ders 800middot843middot3612 From US and Canada All Others Call 920middot426middot59121 Or sendto EAA Mail Orde rsPO Box3086 Oshkosh WI 54903-3086

Lim ited suppli es available middotShipping and handling NOT included Major credit cards accepted WI residents add 5 sales tax

Airplane Banks Shaped like their favorite airplane theyre perfect for the airplane themed bedroom Our banks are made from resin and are handpainted with abright glaze Measures approximately 7 by 7 by 4W Red Mustang $995 52648598 Heliocopter $995 2648597 Biplane $1295 V52652826

Wooden Planes Durable unpainted wooden planes are great for childs play Approximate size is

6 x 45 x 225 inches $449 ea

Airplane Picture Frame Ideal for the nursery or youngsters room decor to display your favorite 4 x 6 photo of the young aviator The picture frame is hand glazed resin and measures about 8 W by 6 34with 3-dimensional clouds and airplanes 52652824

To see more great VAA merchandise go to our website-wwwvintageaircraftorg

Mini Maglitereg Rugged aluminum conshystructed flashlight with

high-intensity light beam from flood to spot with a twist of the wrist Two AA

batteries and a spare lamp inside tail cap

52588216

$1695

300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

And the rest is history

You dont have to be a ma~ician to put the tou~hest easiest-to-repair fabric coverin~ on your pride and joy Just follow the clear detailed instructions in our entertai~ manual Before you can say Hocus-pocus youll have a ~or~eous coverin~ job that you can show off and bra~ about for years to come You dont need a m~ic wand - all you need is Poly-fiber

Friendliest manual around pofyfibercomToll-free technical support information polyfibercom Aircraft CoaUng_80Cgt-361-3490

VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

Something to buysell or trade

Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

MISCELLANEOUS Flying wires available 1994 pricing Visit wwwf1yingwires

com or call 800-517-9278

wwwAeroListorg - Aviations Leading Marketplace

SERVICES Always Flying Aircraft Restoration LLC Annual

Inspections Airframe recovering fabric repairs and complete restorations

Wayne A Forshey AampP amp LA 740-472-1481 Ohio and bordering states

TAiUAlt-66LS

T-CQAFT TAK60PP

AERO CLASSIC COLLECTOR SERIES

Vintage Tires New USA Production

Show off your pride and joy with a fresh set of Vintage Rubber These newly minted tires are FAA-TSOd and speed rated to 120 MPH Some things are better left the way they

were and in the 40s and 50s these tires were perfectly in tune to the exciting times in aviation

Not only do these tires set your vintage plane apart from the rest but also look exceptional on all General Aviation aircraft Deep 832nd tread depth offers above average tread life and UV treated rubber resists aging

First impressions last a lifetime so put these bring back the good times New General Aviation Sizes Available

500 x 5 600 x 6 700 x 8

Oesser has the largest stock and selection of Vintage and Warbird tires in the world Contact us with

continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

152 1 E MacGregor Dr N57W34837 New Haven IN 46774 Oconomowoc W I 53066

260-493-4724 262-560-1949 cl1ief7025(gaoicol1l gdallbueramp-eaaorg

Secretary Treasurer Steve Nesse Charles W Har ris

2009 Highland Ave 72 15 Eas t 46th St Albert Lea M N 56007 Tulsa OK 74 147

507-373- 1674 9 18-622-8400 s171es2009ivtC0111 (whhvsucom

DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

David Bennett Espie Butch Joyce 375 Killdeer Ct 704 N Regional Rd

Li nco ln CA 95648 Green sboro NC 27409 9 16-645-8370 336-668-3650

anl iq llcrinreacl1com wdsockaucom

Jerry Brown Dan Knutson 4605 Hickory Wood Row 106 Tena Marie Circle

Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

Ibrow14906aol coln odicl lbclmrter llet

Dave Clark Steve Krog 635 Vesta l Lane 1002 Heather Ln

Plainfield IN 46 168 Hartford W I 53027 3 17-839-4500 262-966-7627

davecpdf1)attllet sskrogaol co111

John S Copeland Robert D Bob Lum ley 1 A Deacon St reet 1265 South 124th St

Northborough MA 0 1532 Brookfield W I 53005 508-393-4775 262-782-2633

copeland IjIll ICJ(UnI Ill lperexecpccOl

Phil Coulson S H Wes Schmid 2841 5 Springbrook Or 2359 Lefeber Avenue

Lawton M I 49065 Wauwatosa W I 532 13 269-624-6490 41 4-77 1- 1545

rcullisufl 5 16cs(om sltscilmidg11lailcol1J

Dale A Gustafson 7724 Shady Hills Dr

Indian apoli s IN 46278 3 17-293-4430

da lefaycmslcom

DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

Chicago IL 60643 Union IL 60180 773-779-2105 8 15-923-159 1

pllOtopiotaolcom bllck7acsmail com

Ge ne Chase Gene Morris 2 1 S9 Carlton Rd 5936 Steve Court

Oshkosh WI 54904 Roanoke TX 76262 920-23 1-5002 817-49 1-9 110

GRCH ACkllar t er 1let selenlOrrisCw rter l1et

Ro nald C Fri tz 1540 I Sparta Ave

Kent Ci ty M I 49330 616-678-50 12

EAA and Division Membership Services (800 AM-700 PM Monday-Friday CST) 800-564-6322 FAX 92042amp4873 www_ eaaorgjmemberbenefits membershipeaaorg

bullNew renew memberships Address changes middot Merchandise sales Gift memberships

EAA AirVenture Oshkosh 888-322-4636 wwwairventure_org airventureeaaorg Sport PilotLight-Sport Aircraft Hotline 877-359-1232 wwwsportpilotorg sportpiloteaaorg

Programs and Activities Auto Fuel STCs 92042amp4843 dwalkereaaor

Education Aeroscholars 920-426-6570 mrobbinseaaorg bull EAA Air Academy 920426-6880 www_airacademy_org airacademyeaa_org bull EAA Scholarships 920426-6823 scholarshipseaaorg

Rigilt Instructor information 920426-6801 www_eaaorgjnafi tdeimereaaorg Library Services Research 92042amp4848 slurveyeaaorg

Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

EAA Enterprise Rentshy A-Car Program 877-421-3722 www_eaa_orp)enterprise membershipeaaor~

Editorial 920-426-4825 www_ vinta~eaircraft_ or~ vinta~eeaaor~

VAA Office FAX 920426-6579 tbookseaa_org

EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 35: VA-Vol-37-No-11-Nov-2009

300-hp Wright J-6 (R-975) radial The span was 45 feet the overall length was 32 feet 10 inches the gross weight was 3800 pounds and the useful load was 1435 pounds The airspeed range inshycluded a VMAX of 135 mph a Vc of 110 mph and a VMIN of 59 mph Two T-4s were built regisshytered as 898M and NC502V (cn 3 and 4 respectively) During the course of Thadens aircraft buildshying the company had relocated from Oakland and San Francisco to 1625 Island Ave Pittsburgh Pennsylvania By 1929 the comshypany was renamed the Pittsburgh All-Metal Aircraft Co (Pittsburgh Metal Airplane Co Buffington H Glenn Louise Thaden Journal of the American Aviation Historical Society V12 N4 Winter 1967 pp 285-287) and in 1930 became the Metalair Corp a division of the Consolidated Corp (General Aviation Manufacturing Co) Acshycording to AAHS General Motors acquired the company in May ------------------------------shyof 1931 and merged it into Fokshyker before moving it to New Jershysey By this time Louise McPheshytridge had married Herbert von Thaden and was already a highly regarded female pilot of record-setting ability While in Pittsburgh she flew company executives around in either the T-2 or T-4 which was known as The Tin Goslin

While Louise McPhetridge Thadens numerous aeronautical accomplishments are beyond the scope of this work she flew the T-4 (NC502V race number 46) during the cross-country derby from Santa Monica to Cleveland during the National Air Races placing fifth in the womens divishysion In July of 1930 the Thadens had their first child Bill while living at Pittsburgh He was folshylowed by his sister Patsy born at Kansas City in September 1933 The T-1 flew on crashing at Chitna Alaska on 30 March 1933 (Nat Brown subject of a preshyvious Mystery Plane was the pishy

lot) In 1988 William V Thaden Herberts son and a group of EAA volunteers recovered the remains of the T-1 and donated them to the Hiller Museum at San Carlos California

In late December of 2008 I was approached by Mr FT Lovley who had acquired the door of the T-1 from the widow of a bush pishylot who had apparently removed it during the T-1s long rest in Alaska Thanks to the efforts of Mr Dan Hagedorn at the Seattle Museum of Flight the door was identified and is now back with the Thaden family who also have the rudder from the aircraft

In 1967 the Thadens were comfortably living in High POint North Carolina and owned the Thaden Engineering Co which specialized in the development of reinforced plastics Louise M Thaden a charter member of the Ninety-Nines (secretary and vice president from 1931-1932) was

still flying a Staggerwing Beechshycraft Herbert von Thaden died a few years later and was followed by Louise who passed away on 9 November 1979 In 1991 astroshynaut Eileen Collins took Louise Thadens flying helmet into orbit aboard the space shuttle to honor her accomplishments in pioneer womens aviation Louise Thaden was a friend of such noteworthy women in aviation as Amelia Earshyhart Pancho Barnes and Blanche Noyes Her autobiography High Wide and Frightened was reprinted in 2004

Wesley R Smith Springfield Illinois

Other correct answers were reshyceived from Tom Lymburn Princshyeton Minnesota Clarence Hesshyser St Augustine Florida Jack Erickson State College Pennsylshyvania Doug Rounds Zebulon Georgia and Forrest Lovley Jorshydan Minnesota

HARRY HOUDINI LEFT NOTHING TO CHANCE It s all right There s the Pol~-Fiber stamp Go ahead and gveer the gun

And the rest is history

You dont have to be a ma~ician to put the tou~hest easiest-to-repair fabric coverin~ on your pride and joy Just follow the clear detailed instructions in our entertai~ manual Before you can say Hocus-pocus youll have a ~or~eous coverin~ job that you can show off and bra~ about for years to come You dont need a m~ic wand - all you need is Poly-fiber

Friendliest manual around pofyfibercomToll-free technical support information polyfibercom Aircraft CoaUng_80Cgt-361-3490

VINTAGE AIRPLANE 37

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

Something to buysell or trade

Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

MISCELLANEOUS Flying wires available 1994 pricing Visit wwwf1yingwires

com or call 800-517-9278

wwwAeroListorg - Aviations Leading Marketplace

SERVICES Always Flying Aircraft Restoration LLC Annual

Inspections Airframe recovering fabric repairs and complete restorations

Wayne A Forshey AampP amp LA 740-472-1481 Ohio and bordering states

TAiUAlt-66LS

T-CQAFT TAK60PP

AERO CLASSIC COLLECTOR SERIES

Vintage Tires New USA Production

Show off your pride and joy with a fresh set of Vintage Rubber These newly minted tires are FAA-TSOd and speed rated to 120 MPH Some things are better left the way they

were and in the 40s and 50s these tires were perfectly in tune to the exciting times in aviation

Not only do these tires set your vintage plane apart from the rest but also look exceptional on all General Aviation aircraft Deep 832nd tread depth offers above average tread life and UV treated rubber resists aging

First impressions last a lifetime so put these bring back the good times New General Aviation Sizes Available

500 x 5 600 x 6 700 x 8

Oesser has the largest stock and selection of Vintage and Warbird tires in the world Contact us with

continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

152 1 E MacGregor Dr N57W34837 New Haven IN 46774 Oconomowoc W I 53066

260-493-4724 262-560-1949 cl1ief7025(gaoicol1l gdallbueramp-eaaorg

Secretary Treasurer Steve Nesse Charles W Har ris

2009 Highland Ave 72 15 Eas t 46th St Albert Lea M N 56007 Tulsa OK 74 147

507-373- 1674 9 18-622-8400 s171es2009ivtC0111 (whhvsucom

DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

David Bennett Espie Butch Joyce 375 Killdeer Ct 704 N Regional Rd

Li nco ln CA 95648 Green sboro NC 27409 9 16-645-8370 336-668-3650

anl iq llcrinreacl1com wdsockaucom

Jerry Brown Dan Knutson 4605 Hickory Wood Row 106 Tena Marie Circle

Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

Ibrow14906aol coln odicl lbclmrter llet

Dave Clark Steve Krog 635 Vesta l Lane 1002 Heather Ln

Plainfield IN 46 168 Hartford W I 53027 3 17-839-4500 262-966-7627

davecpdf1)attllet sskrogaol co111

John S Copeland Robert D Bob Lum ley 1 A Deacon St reet 1265 South 124th St

Northborough MA 0 1532 Brookfield W I 53005 508-393-4775 262-782-2633

copeland IjIll ICJ(UnI Ill lperexecpccOl

Phil Coulson S H Wes Schmid 2841 5 Springbrook Or 2359 Lefeber Avenue

Lawton M I 49065 Wauwatosa W I 532 13 269-624-6490 41 4-77 1- 1545

rcullisufl 5 16cs(om sltscilmidg11lailcol1J

Dale A Gustafson 7724 Shady Hills Dr

Indian apoli s IN 46278 3 17-293-4430

da lefaycmslcom

DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

Chicago IL 60643 Union IL 60180 773-779-2105 8 15-923-159 1

pllOtopiotaolcom bllck7acsmail com

Ge ne Chase Gene Morris 2 1 S9 Carlton Rd 5936 Steve Court

Oshkosh WI 54904 Roanoke TX 76262 920-23 1-5002 817-49 1-9 110

GRCH ACkllar t er 1let selenlOrrisCw rter l1et

Ro nald C Fri tz 1540 I Sparta Ave

Kent Ci ty M I 49330 616-678-50 12

EAA and Division Membership Services (800 AM-700 PM Monday-Friday CST) 800-564-6322 FAX 92042amp4873 www_ eaaorgjmemberbenefits membershipeaaorg

bullNew renew memberships Address changes middot Merchandise sales Gift memberships

EAA AirVenture Oshkosh 888-322-4636 wwwairventure_org airventureeaaorg Sport PilotLight-Sport Aircraft Hotline 877-359-1232 wwwsportpilotorg sportpiloteaaorg

Programs and Activities Auto Fuel STCs 92042amp4843 dwalkereaaor

Education Aeroscholars 920-426-6570 mrobbinseaaorg bull EAA Air Academy 920426-6880 www_airacademy_org airacademyeaa_org bull EAA Scholarships 920426-6823 scholarshipseaaorg

Rigilt Instructor information 920426-6801 www_eaaorgjnafi tdeimereaaorg Library Services Research 92042amp4848 slurveyeaaorg

Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

EAA Enterprise Rentshy A-Car Program 877-421-3722 www_eaa_orp)enterprise membershipeaaor~

Editorial 920-426-4825 www_ vinta~eaircraft_ or~ vinta~eeaaor~

VAA Office FAX 920426-6579 tbookseaa_org

EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 36: VA-Vol-37-No-11-Nov-2009

EM Calendar of Aviation Events Is NowOnline EMs online Calendar of Events is the go-to

spot on the Web to list and find aviation events in your area The user-friendly searchable format makes it the perfect web-based tool for planning your local trips to afly-in

In EMs onlineCalendar of Events you can search for events at any given time within acertain radius of any airport by entering the identifier or a ZIP code and you can further define your search to lookfor just the types of events youd like to attend

We invite you to access the EM online Calendar of Events at httpwwweaaorgjcalendar

Upcoming Major Fly-Ins US Sport Aviation Expo Sebring Regional Airport (SEF) Sebring FL January 21-24 2010 wwwSport-Aviation-Expocom

AERO Friedrichshafen Messe Friedrichshafen Friedrichshafen Germany ApriiS-ll2010 wwwAERO-Friedrichshafencoml htmll en

Sun n Fun Fly-In Lakela nd Linder Regional Airport (LAL) Lakeland FL Apri l 13-1S 2010 wwwSun-N-Funorg

Virginia Regional Festival of Flight Suffolk Executive Airport (SFQ) Suffolk VA May 22-23 2010 wwwVirginiaFlyinorg

Golden West Regional Fly-In and Air Show Yuba County Airport (MYV) Marysville CA June 11-13 2010 wwwGoldenWestFlylnorg

Arlington Fly-In Arlington Municipal Airport (AWO) Arlington WA July 7-11 2010 wwwArling tonFlylnorg

EAA AirVenture Oshkosh Wittman Regional Airport (OSH) Oshkosh WI July 26-August 1 2010 wwwAirVentureorg

Colorado Sport International Air Show and Rocky Mountain Regional Fly-In Rocky Mountain Metropolitan Airport (BJC) Denver (0 August 21-22 2010 wwwCOSportAviationorg

COPPERSTATE Regional Fly-In (asa Grande Municipal Airport ((GZ) (asa Grande AZ October 21-232010 wwwCOPPERSTATEorg

Southeast Regional Fly-In Middleton Field Airport (GZH) Evergreen AL October 22-24 2010 wwwSERFIorg

For details on hundreds of upcoming aviation happenings including EAA chapter fly-ins Young Eaglesrallies and other local aviation events visit the EAA Calendar of Events located at wwwEAAorgcalendar

3 8 NOVEMBER 2009

Something to buysell or trade

Classified Word Ads $550 per 10 words 180 words maximum with boldface lead-in on first line

Classified Display Ads One column wide (2167 inches) by 1 2 or 3 inches high at $20 per inch Black and white only and no frequency discounts

Advertising Closing Dates 10th of second month prior to desired issue date (ie January 10 is the closing date for the March issue) VAA reserves the right to reject any advertising in conflict with its policies Rates cover one insertion per issue Classified ads are not accepted via phone Payment must accompany order Word ads may be sent via fax (920-426-6845) or e-mail (classadseaaorf) using credit card payment (all cards accepted) Include name on card complete address type of card card number and expiration date Make checks payable to EAA Address advertising correspondence to EAA Publications Classified Ad Manager PO Box 3086 Oshkosh WI 54903-3086

MISCELLANEOUS Flying wires available 1994 pricing Visit wwwf1yingwires

com or call 800-517-9278

wwwAeroListorg - Aviations Leading Marketplace

SERVICES Always Flying Aircraft Restoration LLC Annual

Inspections Airframe recovering fabric repairs and complete restorations

Wayne A Forshey AampP amp LA 740-472-1481 Ohio and bordering states

TAiUAlt-66LS

T-CQAFT TAK60PP

AERO CLASSIC COLLECTOR SERIES

Vintage Tires New USA Production

Show off your pride and joy with a fresh set of Vintage Rubber These newly minted tires are FAA-TSOd and speed rated to 120 MPH Some things are better left the way they

were and in the 40s and 50s these tires were perfectly in tune to the exciting times in aviation

Not only do these tires set your vintage plane apart from the rest but also look exceptional on all General Aviation aircraft Deep 832nd tread depth offers above average tread life and UV treated rubber resists aging

First impressions last a lifetime so put these bring back the good times New General Aviation Sizes Available

500 x 5 600 x 6 700 x 8

Oesser has the largest stock and selection of Vintage and Warbird tires in the world Contact us with

continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

152 1 E MacGregor Dr N57W34837 New Haven IN 46774 Oconomowoc W I 53066

260-493-4724 262-560-1949 cl1ief7025(gaoicol1l gdallbueramp-eaaorg

Secretary Treasurer Steve Nesse Charles W Har ris

2009 Highland Ave 72 15 Eas t 46th St Albert Lea M N 56007 Tulsa OK 74 147

507-373- 1674 9 18-622-8400 s171es2009ivtC0111 (whhvsucom

DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

David Bennett Espie Butch Joyce 375 Killdeer Ct 704 N Regional Rd

Li nco ln CA 95648 Green sboro NC 27409 9 16-645-8370 336-668-3650

anl iq llcrinreacl1com wdsockaucom

Jerry Brown Dan Knutson 4605 Hickory Wood Row 106 Tena Marie Circle

Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

Ibrow14906aol coln odicl lbclmrter llet

Dave Clark Steve Krog 635 Vesta l Lane 1002 Heather Ln

Plainfield IN 46 168 Hartford W I 53027 3 17-839-4500 262-966-7627

davecpdf1)attllet sskrogaol co111

John S Copeland Robert D Bob Lum ley 1 A Deacon St reet 1265 South 124th St

Northborough MA 0 1532 Brookfield W I 53005 508-393-4775 262-782-2633

copeland IjIll ICJ(UnI Ill lperexecpccOl

Phil Coulson S H Wes Schmid 2841 5 Springbrook Or 2359 Lefeber Avenue

Lawton M I 49065 Wauwatosa W I 532 13 269-624-6490 41 4-77 1- 1545

rcullisufl 5 16cs(om sltscilmidg11lailcol1J

Dale A Gustafson 7724 Shady Hills Dr

Indian apoli s IN 46278 3 17-293-4430

da lefaycmslcom

DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

Chicago IL 60643 Union IL 60180 773-779-2105 8 15-923-159 1

pllOtopiotaolcom bllck7acsmail com

Ge ne Chase Gene Morris 2 1 S9 Carlton Rd 5936 Steve Court

Oshkosh WI 54904 Roanoke TX 76262 920-23 1-5002 817-49 1-9 110

GRCH ACkllar t er 1let selenlOrrisCw rter l1et

Ro nald C Fri tz 1540 I Sparta Ave

Kent Ci ty M I 49330 616-678-50 12

EAA and Division Membership Services (800 AM-700 PM Monday-Friday CST) 800-564-6322 FAX 92042amp4873 www_ eaaorgjmemberbenefits membershipeaaorg

bullNew renew memberships Address changes middot Merchandise sales Gift memberships

EAA AirVenture Oshkosh 888-322-4636 wwwairventure_org airventureeaaorg Sport PilotLight-Sport Aircraft Hotline 877-359-1232 wwwsportpilotorg sportpiloteaaorg

Programs and Activities Auto Fuel STCs 92042amp4843 dwalkereaaor

Education Aeroscholars 920-426-6570 mrobbinseaaorg bull EAA Air Academy 920426-6880 www_airacademy_org airacademyeaa_org bull EAA Scholarships 920426-6823 scholarshipseaaorg

Rigilt Instructor information 920426-6801 www_eaaorgjnafi tdeimereaaorg Library Services Research 92042amp4848 slurveyeaaorg

Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

EAA Enterprise Rentshy A-Car Program 877-421-3722 www_eaa_orp)enterprise membershipeaaor~

Editorial 920-426-4825 www_ vinta~eaircraft_ or~ vinta~eeaaor~

VAA Office FAX 920426-6579 tbookseaa_org

EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 37: VA-Vol-37-No-11-Nov-2009

AERO CLASSIC COLLECTOR SERIES

Vintage Tires New USA Production

Show off your pride and joy with a fresh set of Vintage Rubber These newly minted tires are FAA-TSOd and speed rated to 120 MPH Some things are better left the way they

were and in the 40s and 50s these tires were perfectly in tune to the exciting times in aviation

Not only do these tires set your vintage plane apart from the rest but also look exceptional on all General Aviation aircraft Deep 832nd tread depth offers above average tread life and UV treated rubber resists aging

First impressions last a lifetime so put these bring back the good times New General Aviation Sizes Available

500 x 5 600 x 6 700 x 8

Oesser has the largest stock and selection of Vintage and Warbird tires in the world Contact us with

continued from inside front cover

then be required to use the public rulemaking process that is applicable to all other federal agencies Seems fair to me We need to get behind HR 3678 and contact our represenshytatives to let them know this bill is supported by general aviation Locating and communicating with your represhysentatives can easily be accomplished at wwwHousegov houseiMemberWWW_by_Stateshtm

Your EAA Industry and Regulatory Affairs department has done a good job of getting this information out to our membership but the further we spread this type of news the better Please take the time to communicate with your congressional representatives about this imshyportant issue

Remember its time to set your aircraft up for winter operations Its time to get that manual out and review the section on cold-weather operations Winter flying can be a lot of fun but you have to be prepared for it Be safe out there

As always please do us all the favor of inviting a friend to join the VAA and help keep us the strong assoshyciation we have all enjoyed for so many years

EAA AirVenture Oshkosh 2010 The Worlds Greatest Aviation Celebration is July 26 through August l

Ai5

WHAT OUR MEMBERS ARE RESTORING Are you nearing completion of a restoration Or is it done

and you re busy flying and showing it off If so we d like to hear from you Send us a 4-by-6-inch print from a commercial source (no home printers please-those prints just dont scan well) or a 4-by-6-inch 300-dpi digital photo A JPG from your 25-megapixel (or higher) digital camera is fine You can burn photos to a CD or if you re on a high-speed Internet connection you can e-mail them along with a text-only or Word document describing your airplane (If your e-mail program asks if youd like to make the photos smaller say no) For more tips on creating photos we can publish visit VAAs website at wwwvintageaircraftorg Check the News page for a hyperl ink to Want To Send Us A Photograph

For more Information you can also e-mail us at vlntageallclaft eaaolg or call us at 920-426-4825

323-721-4900 FAX 323-721-7888

6900 Acco SI Monlebello CA 90640DESSERlli ~ TelePhone 800-247-8473 or

TIRE amp RUBBER COMPANY 3400 Chelsea Ave Memphis TN 38106 wwwdessercom

VINTAGE AIRPLANE 39

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

152 1 E MacGregor Dr N57W34837 New Haven IN 46774 Oconomowoc W I 53066

260-493-4724 262-560-1949 cl1ief7025(gaoicol1l gdallbueramp-eaaorg

Secretary Treasurer Steve Nesse Charles W Har ris

2009 Highland Ave 72 15 Eas t 46th St Albert Lea M N 56007 Tulsa OK 74 147

507-373- 1674 9 18-622-8400 s171es2009ivtC0111 (whhvsucom

DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

David Bennett Espie Butch Joyce 375 Killdeer Ct 704 N Regional Rd

Li nco ln CA 95648 Green sboro NC 27409 9 16-645-8370 336-668-3650

anl iq llcrinreacl1com wdsockaucom

Jerry Brown Dan Knutson 4605 Hickory Wood Row 106 Tena Marie Circle

Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

Ibrow14906aol coln odicl lbclmrter llet

Dave Clark Steve Krog 635 Vesta l Lane 1002 Heather Ln

Plainfield IN 46 168 Hartford W I 53027 3 17-839-4500 262-966-7627

davecpdf1)attllet sskrogaol co111

John S Copeland Robert D Bob Lum ley 1 A Deacon St reet 1265 South 124th St

Northborough MA 0 1532 Brookfield W I 53005 508-393-4775 262-782-2633

copeland IjIll ICJ(UnI Ill lperexecpccOl

Phil Coulson S H Wes Schmid 2841 5 Springbrook Or 2359 Lefeber Avenue

Lawton M I 49065 Wauwatosa W I 532 13 269-624-6490 41 4-77 1- 1545

rcullisufl 5 16cs(om sltscilmidg11lailcol1J

Dale A Gustafson 7724 Shady Hills Dr

Indian apoli s IN 46278 3 17-293-4430

da lefaycmslcom

DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

Chicago IL 60643 Union IL 60180 773-779-2105 8 15-923-159 1

pllOtopiotaolcom bllck7acsmail com

Ge ne Chase Gene Morris 2 1 S9 Carlton Rd 5936 Steve Court

Oshkosh WI 54904 Roanoke TX 76262 920-23 1-5002 817-49 1-9 110

GRCH ACkllar t er 1let selenlOrrisCw rter l1et

Ro nald C Fri tz 1540 I Sparta Ave

Kent Ci ty M I 49330 616-678-50 12

EAA and Division Membership Services (800 AM-700 PM Monday-Friday CST) 800-564-6322 FAX 92042amp4873 www_ eaaorgjmemberbenefits membershipeaaorg

bullNew renew memberships Address changes middot Merchandise sales Gift memberships

EAA AirVenture Oshkosh 888-322-4636 wwwairventure_org airventureeaaorg Sport PilotLight-Sport Aircraft Hotline 877-359-1232 wwwsportpilotorg sportpiloteaaorg

Programs and Activities Auto Fuel STCs 92042amp4843 dwalkereaaor

Education Aeroscholars 920-426-6570 mrobbinseaaorg bull EAA Air Academy 920426-6880 www_airacademy_org airacademyeaa_org bull EAA Scholarships 920426-6823 scholarshipseaaorg

Rigilt Instructor information 920426-6801 www_eaaorgjnafi tdeimereaaorg Library Services Research 92042amp4848 slurveyeaaorg

Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

EAA Enterprise Rentshy A-Car Program 877-421-3722 www_eaa_orp)enterprise membershipeaaor~

Editorial 920-426-4825 www_ vinta~eaircraft_ or~ vinta~eeaaor~

VAA Office FAX 920426-6579 tbookseaa_org

EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 38: VA-Vol-37-No-11-Nov-2009

Membershi~ Services Directory ENJOY THE MANY BENEFITS OF EAA AND EAAs VI NTAGE AIRCRAFT ASSOCIATION

EAA Aviation Center PO Box 3086 Osh kosh WI 54903-3086 Phone (920) 426-4800 Fax (920) 426-4873

Web Sites IVWWvintageaircratr_org wwwairvetltllreorg wwweaa_orgjmemberbenefits E-Mail vintageaircraleaa_org

VINTAGE AIRCRAFT

ASSOCIATION OFFICERS

Pres idellt Vice-Pres ident Geoff Robison George Daubner

152 1 E MacGregor Dr N57W34837 New Haven IN 46774 Oconomowoc W I 53066

260-493-4724 262-560-1949 cl1ief7025(gaoicol1l gdallbueramp-eaaorg

Secretary Treasurer Steve Nesse Charles W Har ris

2009 Highland Ave 72 15 Eas t 46th St Albert Lea M N 56007 Tulsa OK 74 147

507-373- 1674 9 18-622-8400 s171es2009ivtC0111 (whhvsucom

DIRECTORS Steve Bender Jeannie Hill

85 Brush Hi ll Road PO Box 328 Sherborn MA 01770 Harva rd IL 60033-0328

508-653-7557 8 15-943-7205 sst] ()cam eastlIet

David Bennett Espie Butch Joyce 375 Killdeer Ct 704 N Regional Rd

Li nco ln CA 95648 Green sboro NC 27409 9 16-645-8370 336-668-3650

anl iq llcrinreacl1com wdsockaucom

Jerry Brown Dan Knutson 4605 Hickory Wood Row 106 Tena Marie Circle

Greenwood IN 46 143 Locli W I 53555 3 17-422-9366 608-592-7224

Ibrow14906aol coln odicl lbclmrter llet

Dave Clark Steve Krog 635 Vesta l Lane 1002 Heather Ln

Plainfield IN 46 168 Hartford W I 53027 3 17-839-4500 262-966-7627

davecpdf1)attllet sskrogaol co111

John S Copeland Robert D Bob Lum ley 1 A Deacon St reet 1265 South 124th St

Northborough MA 0 1532 Brookfield W I 53005 508-393-4775 262-782-2633

copeland IjIll ICJ(UnI Ill lperexecpccOl

Phil Coulson S H Wes Schmid 2841 5 Springbrook Or 2359 Lefeber Avenue

Lawton M I 49065 Wauwatosa W I 532 13 269-624-6490 41 4-77 1- 1545

rcullisufl 5 16cs(om sltscilmidg11lailcol1J

Dale A Gustafson 7724 Shady Hills Dr

Indian apoli s IN 46278 3 17-293-4430

da lefaycmslcom

DIRECTORS EMERITUS

Robert C Brauer EE Buck Hilbert 9345 S Hoyne 8 102 Leech Rd

Chicago IL 60643 Union IL 60180 773-779-2105 8 15-923-159 1

pllOtopiotaolcom bllck7acsmail com

Ge ne Chase Gene Morris 2 1 S9 Carlton Rd 5936 Steve Court

Oshkosh WI 54904 Roanoke TX 76262 920-23 1-5002 817-49 1-9 110

GRCH ACkllar t er 1let selenlOrrisCw rter l1et

Ro nald C Fri tz 1540 I Sparta Ave

Kent Ci ty M I 49330 616-678-50 12

EAA and Division Membership Services (800 AM-700 PM Monday-Friday CST) 800-564-6322 FAX 92042amp4873 www_ eaaorgjmemberbenefits membershipeaaorg

bullNew renew memberships Address changes middot Merchandise sales Gift memberships

EAA AirVenture Oshkosh 888-322-4636 wwwairventure_org airventureeaaorg Sport PilotLight-Sport Aircraft Hotline 877-359-1232 wwwsportpilotorg sportpiloteaaorg

Programs and Activities Auto Fuel STCs 92042amp4843 dwalkereaaor

Education Aeroscholars 920-426-6570 mrobbinseaaorg bull EAA Air Academy 920426-6880 www_airacademy_org airacademyeaa_org bull EAA Scholarships 920426-6823 scholarshipseaaorg

Rigilt Instructor information 920426-6801 www_eaaorgjnafi tdeimereaaorg Library Services Research 92042amp4848 slurveyeaaorg

Benefits AUA Vinta(e Insurance Plan 800-727-3823 www_ auaonlinecom EAA Aircraft Insurance Plan 866-647-4322 wwweaa_orgjmemberbenefits membershipeaaorg EAA VISACard 800-853-5576 ext 8884 EAA Hertz Rent-A-Car Program 800-654-2200 wwweaaorp)hertz membershipeaa or~

EAA Enterprise Rentshy A-Car Program 877-421-3722 www_eaa_orp)enterprise membershipeaaor~

Editorial 920-426-4825 www_ vinta~eaircraft_ or~ vinta~eeaaor~

VAA Office FAX 920426-6579 tbookseaa_org

EAA Members Information Une 888-EAA-INFO (322-4636) Use this toll-free number for information about AirVenture Oshkosh aeromedical and technical aviation questions

chapters and Young Eagles Please have your membership number ready whencalling Office hours are 815 am -500 pm_ (Monday -Friday CST)

MEMBERSHIP INFORMATION EAA lAC

Membership in the Experimental Aircraft Current EAA m embers may jo in the Association Inc i5 $40 for one year includshy Inte rnatio n al Aerobatic Club Inc Divishying 12 issues of SPORT AVIATION_ Family sio n and receive SPOR T AEROBATICS membership is an additional $10 annually_ m agaZine for an additio nal $45 per year Junior Membership (under 19 yea rs of age) EAA Membership SPORT AER OBATshyis available at $23 annually_ All major credi t ICS m agazine and o ne year membership cards accepted fo r membership (Add $16 for in the lAC Div isio n is available fo r $55 Foreign Postage) p er year (SPOR T AVIATION magazine

n o t included ) _ (Add $18 fo r Fo re ignEAA SPORT PILOT Postage)

Current EAA m embers may add EAA SPORT PILOT magazine for an additional WARBIRDS $20 per yea r Current EAA members may join the EAA

EAA Me m be rship and EAA SPOR T Warbirds of America Division and receive PILOT magazi ne is availab le fo r $40 per WARBIRDS magaZine for an additional $45 year (SPORT AVIATION magazine not inshy per year_ cluded)_ (Add $16 for Foreign Postage) EAA Membership WA RBIRDS m agashy

z ine and o n e year m embership in the VINTAGE AIRCRAFT ASSOCIATION Warbirds Division is available for $55 per

Current EAA m embers may jo in the year (SPORT AVIATION magaZine not inshyVi ntage Aircraft Association and receive cluded)_ (Add $7 for Foreign Postage) VINTAGE AIRPLANE magazine for an adshyditional $36 per year_ FOREIGN MEMBERSHIPS

EAA Membership VINTAGE AIRPLANE Please submit your remittance with a magazine and one year membership in the EAA check or draft drawn o n a United States Vintage Aircraft Association is available for $46 bank payable in United States dollars_ Add per year (SPORT AVIATION magazine not inshy required Foreign Postage amount for each cluded)_ (Add $7 for Foreign Postage) membership_

Members hip dues to EAA and its divisions are not tax deductible as charitable contributions

Gopyright copy2009 by the EAA Vintage Aircraft Association All rights reserved_ VINTAGE AIRPLANE (USPS 062-750 ISSN 0091-6943) is published and owned exclusively by the EAA Vintage Aircraft Association of the Experimental Aircraft Association and is published monthly at EAA

Aviation Center 3000 Poberezny Rd_ PO Box 3086 Oshkosh Wisconsin 54903-3086 e-mail vintageaircrafteaaorg Membership 10 Vintage Aircraft Associalion which includes 12 issues of Vintage Airplane magazine is $36 per year for EAA members and $46 for non-EAA members_ Periodicals Postage paid at Oshkosh Wisconsin 54901 and al additional mailing offices POSTMASTER Send address changes 10 Vinlage Airplane PO Box 3086 Oshkosh WI 54903-3086_ PM 40063731 Return undeliverable Canadian addresses 10 Pilney Bowes IMS Stalion A PO Box 54 Windsor ON N9A 6J5_FOREIGN AND APO ADDRESSES - Please allow al leasl two months for delivery of VINTAGE AIRPLANE to foreign and APO addresses via surface mail ADVERTISING - Vintage Aircraft Association does nol guaranlee or endorse any product offered through the advertising We invite constructive criticism and welcome any report of inferior merchandise obtained through our advertising so that corrective measures can be taken

EDITORIAL POLICY Members are encouraged 10 subm~ stories and photographs Policy opinions expressed in articles are solely those of the authors_ Responsibility for accuracy in reporting rests enlirely with the conlributor_ No remuneration is made Malerial should be senllo Ed~or VINTAGE AIRPLANE PO Box 3086 Oshkosh WI 54903-3086 Phone 920-426-4800_

EAAreg and EAA SPORT AVIATIONreg the EAA Logoreg and Aaronautica middot are regislered tradematllts trademarks and service marks of the Experimenlal Aircraft Association Inc The use of Ihese tradematllts and service marks wrthout the permission at the Experimental Aircraft Association Inc is strictly prohibited

40 NOVEMBER 2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 39: VA-Vol-37-No-11-Nov-2009

bull bull bull bull

Drive one

bull Available voice-activated SYNC entertainment Drive Smart I

Its Not Just a Pickup Truck Its a Ford F-150Vehicle Health ReRort

201 0 Ford F-150

LIN COL N MERCURY

bull A6-speed automatic transmission with TowHaul Mode

bull Best In Towing

bull Voice-activated Ford SYNCregSystem plus 911 AssisfM

bull Six Standard Airbags

bull Five-star ratings from the National Highway Traffic Safety Administration

Page 40: VA-Vol-37-No-11-Nov-2009