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regers g{:(D,lf,, fnc,3418 Cypresswood Dr., Spring, TX77388Office 287 -482-0228 Fax: 281 -355-56 1 5
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$TSPTCTION REPORT & TOGBOOK ATTACHMTNT
CUST: STARFLITE AVIATION9OOO RANDOLPHHOUSTON, TX 77067
ATTN: Chief Inspector
LOCATION: HOU- HOBBY
Item Description:AIRPLANE: WESTWIND 1 124
Desc.ription of WorkPERFORM NDT ONLY I.A.W. THE FOLLOWING:1) EDDY-CURRENT INSPECT MAIN & NOSE LANDING GEAR PIVOTS, SUPPORTS AND TRUNNIONSAFTER OFF-TAXI-WAY EXCURSION PER CUSTOMER REQUEST.
NOTE: INSPECTION PERFORMED IN-SITU AND NO OPEN UP OR OTHER PREPARATION WASPERFORMED EXCEPT FOR LIGHT CLEANING OF GENERAL AREAS.
Results:NO DISCONTINUITIES FOUND AT THE TIME OF THIS INSPECTION
DATE: L2/2/2oo4WO: 9892PO: 83$c- l2-A4
REG: N83SG
TYPE: LI24SN: 368
TTA: 8676.8
LDGS: 6254
1,Wallace W. Warren
Chief InspectorPage 1 of 1
FAA CRS XW1R627K
regers g{O,{,, Inc,3418 Qrpresswood Dr., Spring, TX77388Oflice 281-482-A228 Fax: 28 1-355-56 ls
E - mail : -*::i$: 1_q ie.r't' *i 33., ii,i i;.j i r a tr $ ;ia :3 " r-l" <; i:
CUST: STARFLITE AVIATION
9OOO RANDOLPHHOUSTON, TX 77061
WORI( ORI}ER
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3892DATE: 12 /2 /a4
83Sc- 12-O4P.O. NO.
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Iils"rRucTlolts AIRPLAM: WESTWIND 1 124
PART ITAUE unc. IAIs/tr369 RtGN83SG TYru 1 124 P/r rrAg676.g LDas 6254X INSTRUCTIONS CONTTNUED I IREMARKS
PERFORM NDT ONLY I.A.W. THE FOLLOWING:1) EDDY-CURRENT INSPECT MAIN & NOSE LANDING GEAR PIVOTS, SUPPORTS AND TRUNNIONS AFTER
FF-TAXr-WAY EXCURSION pER CUSTOMER REQUEST.
NOTE: INSPECTION PERFORMED IN-SITU AND NO OPEN UP OR OTHER PREPARATION WASPERFORMED EXCEPT FOR LIGHT CLEANING OF GENERAL AREAS.
DATE COTPLETED
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NO APPARENT DISCONTINUITIES WERENOTED ATTHETIME OF INSPECTION
INSP. REL.
LOG ENTRY OR ATTACHMEI\ITNO AIRWORTHINESS DETERMINATIONMADE BYTHIS INSPECTION
INSP. REL. FOR MORE TFIANONE PART OPTHE SAME S/N UNM.
SEE ATTACHED
SEE REVERSE
I
L{ ::Wallace W. Warren
Chief Inspector
Page 1 of 1
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TIRE S/N: 42961159 CIF
THE ABOVE COMPONENT WAS OVERHAULED IN ACCORDANCE WITH THEMANUFACTURERS OVERHAUL MANUAL. WE PERFORMED THE FOLLOWINGINSPECTIONS.
DISASSEMBLE, CLEAN, STRIP, VISUAL INSPECTION, EDDY CURRENT INSPECTION,FLUORESCENT PENETRANT INSPECTION, MAGNETIC PARTICLE INSPECTION,TREAT, PAINT, REASSEMBLE, PRESSURE TEST AND BALANCED.
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(New unless otherwise stated)16X4.4-4PLY13830-2062913889-20629RG5MS2B775-261c4vc51%OZ.1o2.
GDY. TIRE PN: 164F43-2 C/FCUPCONEGROMMETPACKINGCORECAPWEIGHTSWEIGHTS
THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OFTHE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TOSERVICE. THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVEMUST BE STORED IN COMPLIANCE WITH MANUFACTURERS'SPECIFICATIONS.*PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THE REPAIR STATION UNDER
405 NEBMSKASOUTH HOUSTON, TX 77587FAA REPAIR STATION NO. XVIR626K
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TIRE S/N: 42961118 CIF
THE ABOVE COMPONENT WAS OVERHAULED IN ACCORDANCE WITH THEMANUFACTURERS OVERHAUL MANUAL. WE PERFORMED THE FOLLOWINGINSPECTIONS.
DISASSEMBLE, CLEAN, STRIP, VISUAL INSPECTION, EDDY CURRENT INSPECTION,FLUORESCENT PENETRANT INSPECTION, MAGNETIC PARTICLE INSPECTION,TREAT, PAINT, REASSEMBLE, PRESSURE TEST AND BALANCED.
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GDY. TIRE PN: 164F43-2 CIFCUPCONEGROMMETPACKINGCORECAPWF.IGHTS
THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OFTHE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TOSERVICE. THE AIRCRAFT COMPONENT OR APPLIANCE ]DENTIFIED ABOVEMUST BE STORED ]N COMPLIANCE WITH MANUFACTURERS' SPECIFICATIONS.
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TIRE S/N: 41560920 C/F
THE ABOVE COMPONENT WAS OVERHAULED IN ACCORDANCE WITH THEMANUFACTURERS OVERHAUL MANUAL. WE PERFORMED THE FOLLOWINGINSPECTIONS.
DISASSEMBLE, CLEAN, STRIP, VISUAL INSPECTION, EDDY CURRENT INSPECTION,FLUORESCENT PENETRANT INSPECTION, MAGNETIC PARTICLE INSPECTION,CORROSION CONTROL WORK, REPAIRED RIVETS ON DRIVE KEY AREA, TREAT,PAINT, REASSEMBLE, AND PRESSURE TEST.
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THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OFTHE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TOSERVICE. THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVEMUST BE STORED IN COMPLIANCE WITH MANUFACTURERS'SPECIFICATIONS.*PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THE REPAIR STATION UNDERWORK ORDER NO
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TIRE S/N: 41560914 C/F
THE ABOVE COMPONENT WAS OVERHAULED IN ACCORDANCE WITH THEMANUFACTURERS OVERHAUL MANUAL. WE PERFORMED THE FOLLOWINGINSPECTIONS.
DISASSEMBLE, CLEAN, STRIP, VISUAL INSPECTION, EDDY CURRENT INSPECTION,FLUORESCENT PENETRANT INSPECTION, MAGNETIC PARTICLE INSPECTION,CORROSION CONTROL WORK, REPAIRED RIVETS ON DRIVE KEY AREA, TREAT,PAINT. REASSEMBLE. AND PRESSURE TEST.
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THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVE WAS REPAIREDAND INSPECTED IN ACCORDANCE WITH CURRENT MAINTENANCE RULES OFTHE FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RETURN TOSERVICE. THE AIRCRAFT COMPONENT OR APPLIANCE IDENTIFIED ABOVEMUST BE STORED IN COMPLIANCE WITH MANUFACTURERS' SPECIFICATIONS.--PERTINENT DETAILS OF THE REPAIR ARE ON FILE AT THE REPAIR STATION UNDERWORK ORDER NO.
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E-MAIL : unitedbatteries@aol. comFORM #900?
NiCad Battery Pack Work Order #-7801
Customer;$!ggl!!!1 Date Received -10/19/04 Customer PO#
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FORM #9007NiCad Battery Pack Work Order #_7502
Customer-$!gg[!!!9_ Date Received 10/19/04 Customer PO# N83SGBattery Pack/Cell/Power Supply Mfg. Jet Mfg. Type
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lnspector Recommendations -Thi aircraft component, appliance or accessory was lnspected in accordance with the current requirements of the.
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.,uthorized Inspection Signature
in accordance with the current requrements or melnspector Recommendation s
Date of Final Inspection for Retum to Service
return to
M"irte*tA Release Issued YES or No
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LOG # 2253STARFLITE AVIATION
DAILY AIRCRAFT & ENGINE LOG Dzc "{)AIR.RAFT *o. A,/f3sq
___qYqllsFORWARD
rHiS Loc
TOTAL
67L
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I-AST MAINTENANCE PERFORMED
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LOT i LOG BYYING I
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FLr3591
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NEXT INSPECTION
FUEL PURCHASE LOG
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1. ApF )g National Aviation
Autl. -YlclountyiFAA/'LINITED STA1 lls
2. AUI'HORIZED RE- IASE CERTIFICATEFAA F'orm 8130-3. AIRWOI'-THINESS APPROVAL TAG
3. Form Trackine fber:
20765
4. Organization Name and Address: Repair Station# T4XR853J
TEXAS PNEUMATIC SYSTEMS, INC.2404 SUPERIOR DRIVE, ARLINGTON, TEXAS 76013, FAX 8171795-3474,8171794-0068
5. Work Order/Contract/Invoice Number
40372 I 0082s8-00
6. ltem 7. Descriptior: 8. Part Nu.mber: 9. Eligibility:* 10. Quantitl I l. Serial/Batch Number 12. Status/Work:
I VAI,VE 3213894-4-l N/A I P-234 OVERHAT]LED
13. Remarks: Description of the work performed is attached as form 100 for the article listedin blocks 6, 7, 8, l0 and l l as applicable. All documents included and referenced
are on file at the abov€ r€f€renced organization under the work order and system
tracking reference number indicated in blocks 3 and 5.
Notice: An airworthiness directive may apply to the article(s) described hereon.The installer is r€sponsible for ensuring complete compliance with any applicableairworthiness directiYes.Maintenance, preventive maintenance and/or Alterations have be€n performedwith refer€nce to: Manual 36-13-21. dated Nov 4.1996. Rey# 2.
19. TXI 14 CFR 43.9 Retum to Servrc€ Other regulation specified in Block 13
Certifies that unless otherwise specified in Block 13, the work identifred in Block12 and described in Block 13 was accomplished in accordancc with Title 14, Code
ofFederal Regulations, part 43 and in respect to that work, the items are approvedfor retum to service.
20. AuthonzedSignatwe:*z 21. Approval/Certrficate No.:T4XR853J
It is imp(work in i
the user/
Statemcrwith nati
FAA f.o
UserAnstaller Re
ffi enaato-net-oesnoaautomatLtltilccordance with the national regulations ofan Airworthiness Authority different than tnstaller ensures that his/her Airworthiness Authoriq' accepts parts/componcnts/asseml
Its in block l4 and l9 do not constitute installation ccfiification. In all cases aircraft nr
onal regulatjons by thc uscr/installer before thc airclaft may bc flown.
rm 8tj0-f (64D -lnsraller must cross-r+reck ellr
22. Name: (T)?ed or Printed) | 23. Dut. (m/d/v):I
TL DRAKE I Mav 7.2004t''! ponsrDllrrcsi n-srriurc,rurl'olrio |n-_illTrtre @hr Arrworthiness Authority ofthe countfy specified in block t, it is essential that
'lies from the Airlvorthiness Authority ofthc country specified in block L
hrntcnance records must contain an installation ccftification issucd in accordance
, \ryORK ORDER FORM lOO. TEXAS PNEUMATIC SYSTEMS,INC.
' 2404 SUPERIORDRTYEARLINGTON, TEXAS 76013
,t79+0068
Customer: AERPNE / AERO PNEIIDRAULICS, INC.Cust RO#:008258-00 SIep:COMPLETEWork Req:FUNCTIONAL
PA[: 3213894-4-1 / VALVE sa[: P-234
Page No.
FAAcRSJill|lililruruU[|illwoRK ORDER:40372'04
Dept#:VA Location:
WarrantyCode:00 / 0
Goodthru AD#:
Mfg:[IOll"WE HONEYWELL
HTDDEN
N/A
Manual#: 0802 RewDate: Now 4,L996 Rewf : 2
Reason,/Fun:
UNKNOWN
Date Reqrd: Mar LO,2OO4 Date Estmtd: May 6,2904
RECEMNG: DATE: Feb 5,2OO4 INSPECTED BY: EMMIIT BRACEY
NO VISIBLE DAlilAGE.ttNIT RECEI\IED MfSS I.D PLATE PLE:ASE I.DP/N AND s/N FRoM PAPER woRK UNIT MISSING ID PI.ATE
TNCoMING P/N 3213894-4-L, S/N P234
PRE TEST : DATE: Feb 9,2OO4 TESTED BY: SCOTT DEVEIIDER
UNIT TATI,ED PRETEST. FLOW MIXING POPPET, EXTERNAL A}ID CHECK VAL\IE
IJEAKAGE IS TO HIGH
TEARDOITN FINDINGS:01. 1008 KrT RE9UTRED
02. BALL VALVE SEAT NICKED
03. Mrsc. !{ARD}IARE REQUIRED
04. SENSING PROBE SILTER CLOGGED.
TECHNICIAIT : CHRIS KIDI|ELL DATE: Feb 16,2OO4
FINAL INSPECTION BEFORE ASSEMBLY: DATE: !!ar 24,2OO4 INSPECTED BY: CHRIS KIDIIELL
CORRECTIVE ACTION:
01. REPLACED 1OO8 KIT.02. REPLACED BALL VAL\IE SEAT.
03. REPI.ACED MISC. HARDWARE.
04. REPI.ACED PROBE.
TECHNICIAIiI:CHRIS KIDI|ELL DATE: Mar 25,2OO4
MODIFICATION/ SERVI CE BUI.I.ETINS :
N/A
Test Data Used: 36-L3-2L REV.2 LL/4/95\est Tectrnician: RICK FISK DATE: May 6,2004
-inal Inspeetion: DATE:
ADDITIONAL COMMENES:
ouTGorNG P/N 3213844-4-L, S/N P-2347 3:56:55 4H37001
woFm
,2004May Lab or rask contro'I# | llllll lllllll lll llll llllllll ll llllllll llll lll llll
AERO PNEUDRAULICS, INC25930 BELLE PORTE AVENUEHARBOR CITY, CA 90710
lPhone: (310)891-0300
FAX: (310)891-1248
FAA# O5PR282Y ARINC: THIRTY DAYS
. DATE,RECEIVED WORK ORDER NO.
. DATE COMPLETED ''CUSTOMER ORD NO.
B
I
L
L
T
w3225WORTHINGTON AVIATIONPO BOX 217172995 LONE OAK CIRCLE, SUITE 1O
EAGAN MN 55121
S
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To
w3225WORTHINGTON AVIATIONPO BOX 217172995 LONE OAK CIRCLE, SUITE 1O
EAGAN MN 55121
WARRANTY REPAIR 3213894-4-1 VALVE, REGULATING P-234
.., , i,,'i:'; Cus,lgrner Paqhlo. ,4 tt:
36-13-21
,,:ai :i$l L
20207-022 11t04t1996
CALIBRATE.
NO EXTERNAL DEFECTS NOTED
SENT TO TEXAS PNEUMATICS FOR OVERHAUL
UNIT WAS OVERHAULED BY TEXAS PNEUMATIC.
Service Performed
flAccented [Denied l--lun
GARY FURLONG
m-L
"r'&rta.t
Worthington Aviation PartsoP.O. BOX 217172995 LONE OAK CIRCLE, SUITE 1O
EAGAN, MN 55121, USAPh: (651) 994-1600 Fx: (651) 393-3310Web : www.worth in gtonav.com
Inc.
Email: worthinqtonav.com
Packing SlipSO #: 19949 Original
Date Printed: 1Ol7 12004
Time:5:09:37 PM# of ltems: 2
Page:1
To:START'LITE AVIATION9OOO RANDOLPHHOUSTON. T){7706IUSAATTN: DAVID
Ship To:STARFLITE AVIATION9OOO RANDOLPHHOUSTON. TX77O6IUSA
Date Open:101712004 Ship Via: FED X P1
Customer #:STARFLITE Ship Via Acc:25354007-9Customer PO#: N83SG
Buver: DEWEY R. SMITH
|.'$ffi1
2
32138944.1 VALVE, BLEEDSerial#:P-234
]ustomer Reference: N83SG
I Exchange Information ]Core Due:111612004
Core Charge:$O.OO Core Credit:$0.0OCore PN:3213894-4-1 Core SN:
214001 KIT BLEED SWITCH VALVE INSTALL
lustomer Reference: N83SG
10t7t20w
10t7t2004
4I
1
OH
OINE
THANK YOU FOR THE ORDER
enesbitt@worth in gtonav. com
Authorized Signature:
Thank you for your business. Pleasevisit us online at
www.worth i n gto nav.com
Value Added Customer Service
SI'tt't
GENERAL OYNAMICSAviation Services'
REF. DOCUMENT: Sales orderpAcKlNc LISTNUMBER. 2795J-39
GAC REP:CARRIER:
CARRIER ACCT:
FRT TERMS:FOB POINT:
WAYBILL:
SHIP DATE:
61_4rA
PHONE: 92O-735- 7000FAX: 920-735-7108
FRT CHRG:
PAGE: 1DArE: o8 / 1-2 / O4
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CERTIFICATION OF CONFORMANCErified on this shiomr net the conditions of this sl* order Sellq linhs cenifis. or hs ..o file its supplir cenification. that lhese were
Seller hercby cenifi6 or ho on file irs suppliq's cenification, that thc pd rnd/or componsts idfrlified on this shipp€r ilet th€
dctcrrnindiobcinconfirnnancervithappiicablespecificati<98nd-4rc-considsedtobcin-cotnpliance'...,shipped ourside lhe Unitei Srata. Sellq or Sells's manufactur( or supplifl cdifi.s lhal such pans and cornponenls conpll $ith produclion requirclnenls
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GENERAL CWNAMICSAviation Services'
REF. DOCUMENT: Sa].es OrderPACKTNG LIST NUMBER. 27 95202
GAC REP:CARRIER:
CARRIER ACCT:
FRT TERMS:FOB POINT:
WAYBILL:
SHIP DATE:
6145A' PAGE: 1DArE: 08 / 12 / 04
FRoM
21_4-902-750021-4-350-5560
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HAZARDOUS: ,,
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GASI(ETGASKETGASI(ETSCREW
3228 NEIL flBMSTNONE BOULEVNND EnEnN. MN 58,21 rEL: EEI -gs4- I EOO Fnx: EEl.9S4-O500
FOR:
P.O. #
QTY.
CORRU-SEALS. INC.
24 CAPITAL DRIVEWALLINGFORD. CONNECTI CUT O 6492
TELEPHONE: (203) 265-9331FAX: (203) 269-1023
" WEB: WWW.CORRU-SEALS.COMEMAIL: [email protected]'NET
CERTIFICATE OF CONFORMANCE
GULFSTREAM AEROSPACE
7440 AVIATION PLACE
FAA REPAIR STATION VJIR56OK
DALLAS, TX75235
D6664045Q
DATE:
PART #
JOB NO. 67618
REV. #
85
IT IS HEREBY CERTIFIED THAT ALL MATEzuALS USED IN TFM MANUFACTURE OF THE PARTS FOR THIS
PURCIIASE ORDER CONFORM TO TF{E MATERIAL SPECIFICATION CALLED FOR.
WE FURTHER CERTIFY TT{AT THE MATERIAL TEST REPORTS AND PROCESS CERTIFICATIONS ARE ON FILE
AND SUBJECT TO YOUR EXAMINATION AT OUR PLANT.
_QUIpN,{Eff CONTATNTNG rurencunv oR MERCT/RY coMpouNDS wAS NOT USED FOR FABRICATIONS'
ASSEMBLY, PACKAGING, INSTALLATION, EXAMINATION, OR TEST'ING OF PARTS OR ASSEMBLERS ON THIS
ORDER. *
wE CERTIFY THE ITEMS HAVE BEEN FABRICATED TO TI{E PRODUCT DRAWING'REQUIREMENTS AND FULLY
CONFORM TO TFM SPECIFICATIONS DEFINED IN THIS PURCHASE ORDER OR APPJ-ICABLE PROCEDURES'
\./ - h-SHIPMENT C6MPLETp X PARTIAL SHIPMENT
MATERIAL: AMS 5510P BY
FIEAT TREAT: ANNEAL TO AMS 55IO BY METALLURGICAL PROCESSIN9:
HARDNESS:
PLATE/COAT:
N.D.T.: N/A
N/A
.^ 722-=+-a-'
F.T. GOODYEARQUALITY CONTROL, MANAGER
FORM 185-2
iltilry.1wt:l-^:l
REV.: 6/1i00
WORKORDERFORM lOOTEXAS PNEUMATIC SYSTEMS, INC.2404 SUPERI'CRDRTVEARLTNGTON, TEXAS 76013
/F|{ 817/795-3474'79+0068
Customer: AERPNE / AERO PNEIIDRAULICS' INC.Cust RO#:008258-00 SIeP:COMPLETE
Work Req:FUNCTIONAL
P/r{: 3213894-4-1 / VALVE S/N: P-234
Page No.
FAA cRS Jilil llllil|flruuuulllllil
woRK oRDER:40372-04
Dept#:VA Location:
WarrantYCode:00 / 0
Goodthru AD#:
Mfg:HOIYWE HONEYWELL
PARTS DETAII.:Line# Part Nqmber/Description W CD RrrvCde Qty Unit Price Ext. Price
1 100s KrT1C0t iirt
2 3169884-1SENSING PROBE
3 9674LO-2SE.AT
4 Ms24693C273scREll
1.00 L119.23 LL79.23
1. 00 7 48 .75 7 48 .75
1.00 560.00 560.00
FEDERAL AYIATION ADMIIVSTRATION, AI{D
TEIS REPAIR STATION.
Approved for Return to Service by
WAS OVERIIAIJLED IN ACCORDAI{CE WITE TIIE CTIRRENT REGIILATIONS OF THF',
TO SERVICE. DETAILS ARE ON FILE AT
MAINTENANCE RELEASE RECORI)
artsLabor Total
2488.29450.00
PRICE 2938.29
. GARRETT AVIATION SER\/ICES, 54340 . OO STAR FLITE MANAGEMENT GROUP
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ISS REV DATE
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CM / LEFT ENGINE COMPUTER
.JOB CARDNR/000000001
w/o DATE10 /rL /2004
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MCH I INSAPPROVED DATA REF
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[INITED BATTf,RIES AND ACCESSORIES, INC.CRS #U9BR6 1 8Y 7 7 62 BRANIFF HOUSTON , TX 7 7 06I
TEL: 713 991-91I I FAX: 713 991-91,17
E-MAIL : unitedbatteries@aol. cornFORM #900?
NiCad Battery Pack Work Order #-zu,!-
Customer-,$1gg.@ Date Received --!-0@94- Customer P0# LoanerBattetf Pack/Cell/Power Suoolv Mfe. Jet
Serial No. 4935
Mfg. Type PS-E328 Mfg. PaFNo. 501-107S02
Pre-Service Hidden Damage Inspection
General Condition V*' ry.hSReceiving Voltage: Terminals Battery Pack#l
Battery Pack#2fuzCt;itnrrri@^ses@
ReceptacleAssy. ,2.r2 > s1I^@ l0 Amp Fuse
In-service Ilidden Damage InspectionCaoacitv Tests. Step I throueh 3
ffi*',
I lrst* End of Dischar
End of Discharge VoltageFINAL CHARGE
End of Charge Terminal VoltageFunctional TestReplacedRemarks
WARRANTY:
-Work Accomplished
Inspected B
diie of return to service if serviced a minimum of every 6 months.
evn\d fa'ecompletion out" la */g - o /
per
lnspector RecommendationsThi aircraft component, uppliu*. or um*ry was inspected in accordance with the current requirements of the
Federal Aviation Administration and is approved forPertinent details are on file at this repair station.
Authorized Inspection SignatureDate of Final Inspection for Return to Service
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IINITED BATTERIES AND ACCESSORIES, INC.CRS #U9BR6I8Y 7762 BRANIFF HOUSTON, TX 77061
TEL: 713 991-9111 FAX: 713 991-9117E-MAIL : un i tedbatteri es(glao l. com
FORM #9007NiCad Batterv Pack Work Order # 7795
Customer Star Flite Date Received __10/18/91_ Customer PO# LoanerBattery Pacli/Cell/Power Supply Mfg. Marathon Mfg. Type
Serial No. NiA
Mfg. Part No. 3E451-004
P re-Service Hidden nyaBe Inspection
General Condition YP. C)4'wrr-"\Receiving Voltage: Terminals &5 gt Battery Pack#l lzPack
2 - Battery Pack#ZOuter Case /zV /Circuit Board </rf Censl0enCases ,?r-z S Hot Spots A(e N ?Receptacle Assy. 5 Amp Fuse l0 Amp FuseIn-Service Hidden Damage Inspection
End of Di
End of Discharse VoltaeeFINAL CHARGE
4th ,,6o l'Aa /.1o vlkr ,4, b,</,i rA 4End of Charge Terminal Voltage 3e.', cr
Functional TestReplacedRemarks
WARRANTY: Months from date of return to service if serviced a minimum of every 6 months.
Work Accomplished !y per CMM
Inspected By
Inspector RecommendationsThe aircraft component, appliance or accessory was inspected in accordance with the current requirements of the
Federal Aviation Administration and is
Pertinent details are on file at this repair stqli
Authorized Inspection SignatureDate of Final Inspection for Return to Service
return to serylce.
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1. Apprroving Nahuthority/C
FAIVUNITED
4. Orgarlzation NaColumbia .a,vionics, lr
I rND-
ional Aviati,ln | 2.cuntry: I STATES
AUTHO. .,ZED RELEASE CERTIFICATEFM FORM 813G3, AIRWORTHINESS APPROVAL TAG
ne andAdcress.c. - 11200 /,irport Road - Columbia, MO 65201
3. Form Tracking Number. ^,
5. Work Order, Contract, or InvoiceNumber:
4911
Descriptiorr: 8. Part Number: 9. Eliqibllitv:* 10. Quantity: 11. Serial/Batch Number: '12. StatusMork:
100 622-433't-Oo',l N/A 1 1253 Tested
13. REM,A,RKSTested unit to lvlFR s recifications.
C;ertifies ttrat tfre w.ori: specified irr block 1 2/13 was carried out in accordance with JAR-145 and in respect to that work the aircraft component is considered ready forrr:k:as'-. to service un,ler JAA Acceptance Certificate Number JAA-5631 .
19. El 14 cFR 43.9 Return to Service E other regulation specified in Block 13
Certifies that unless otherwise specified in Block 'l 3, the work identified in Block 12 and
described in Block 13 was accomplished with Title 14, Code of Federal Regulations,to the work. the items are for return to service.
21. ApprovallCertificate No:
23. Date (midly):
0912012004
104N
User/l nstal ler Responsibilities
It is important to und€,,rstand that .he existence of this Document alone does not automatically constitute authority to install the parUcomponenVassembly.
Where the user/instatler perforrns works in accordance with the national regulations of an airworthiness authority different than the Airworthiness Authority of thecountry specified in 3lock 1 it is essential that the user/installer ensures that his/her airworthiness authority accepts partsicomponents/assemblies from theainrrofthine:;s aruthority of the country specifiedin Eiiock 1.
S,tatementsinB|ocks14and19lonotconstituteinsta||ationcertification.|na||cases,aircrafmaintenancerecordsmustcontainaninsta||ationceifcat|onlssuedin accordiarrce with tha national r€igulation by the user/installer before the aircraft may be flown.
FAA Forrn 8130-3 (6-01) * Installer must cross check eligibility
regers fi{:(D,f,, fnc,3418 Cypresswood Dr., Spring, TX77388Office 28I-482-0228 Fax: 28 1 -355-56 1 5
E-mail: i":,+'ii{ i;.n';;.-,i i-:,*?1 :: ;'t::;;::;.:::1.:,,.;"i..1.ra.*-:?
INSPECTION REFORT & LOGBOOK ATTACHUTNT
CUST: STARFLITEAVIATION9OOO RANDOLPHHOUSTON, TX 77061
ATTN: Chief Inspector
LOCATION: HOU- HOBBY
Item Description:AIRPLANE: WESTWIND 1 124
Descriptioa of WorkPERFORM NDT ONLY I.A.W. THE FOLLOWING:A.D.2004-L4-|4 & S.B. Lr2+-55-L50
RADIOGRAPHIC INSPECT RUDDER ONLY I.A.W.
DATE: 9/27 /2044WO: eB$ZPO: 83S$-09-O4
REG: N83SG
TYPE: II24ASN: 368
rtn: E(?S, /LDGS: 4Z P /
Results:NO DISCONTINUITIES FOUND AT THE TIME OF THIS INSPECTION
'Wallace W. Warren
Page 1 of 1
FAA CRS XM1R627KChief Inspector
BILLIITG IIINORilATIOII ]
INVOICE NO. i4SS
DATE ae!271o4 1
CUST: STARFLITE AVTATION
9OOO RANDOLPHHOUSTON, TX 7746I
fugers IV:(D,{,, fnc,3418 Cypresswood Dr., Spring, TX77388Office 281-482-0228 Fax: 28 1-355-56 15
E-mail : nE;.a:ar igr. ili.;: ;i .,:: ii. r,, {: j i:, ii il E;a j.i, ;i * r
WORK ORDER
$ss2DATE: 9/27 lO4
83SG-S9-04wREQ #
ffi FoLLowING: RADIoGRAPHIC INSPECT RUDDER ONLY I.A.W.
D.2AA+-I4-14 & S.B. 1124-55-150
NO APPARENT DISCONTITTUTflES WERENOTED AT THE TIME OF INSPECTION
INSP, REL.
Loc ENrRY o - a/'4/o"*7/2/ryNO AIRWORTHINESS DEIERMINATIONMADE BYTHIS INSPECTION
INSP. REL. FOR MORE THANONE PART OFTHE SAME S/N UNIT.
EE
SEE ATTACHED
-I I sBB REVERSE
IrsrRuerlol{s AIRPLA}IE: WESTWIND 1 124
PART trATI tre. IAIs/tr369 IIE'GNS3SG TYI'E 1 l24A P/If n^ &(/,, t '*'{zrot /X i TNSTRUcTIoNS cot{TINUED REMARKS
DATE @TPT,ETED
Chief Inspectuf
Page 1 of 1
FAA CRS XW1R627K
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regers g{:(D,tf,, fnc,3418 Cypresswood Dr., Spring, TX77388Office 281-482-0228 Fax: 28 1-355-56 15
E-mail: t,\: ":":
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WORI( ORDERCUST: STARFLITE AVTATION
9OOO RANDOLPHHOUSTON, TX 77067
I BrLLulG rilroRuATroniINVOICE NO. r.n?5
8839DATE: 8l r8/o4
*3S{i_rftt_{"}4P.O. tO.
REQ #
IIi| TRUSI-I(,IIS AIRPLANE: WESTWIND 1 124
PART TATE urc. IAIs/tr369 FE(iNS3SG TYFE 1 l24A P/r rrA8605.9 LD(rIr6203
X I INsrRUcrroNs coNTTNUED REMARKS
RFORM NDT ONLY I.AW. THE FOLLOWING: IAI NDT MANUAL PART 2.27-1A-oO RADIOGRAPHICNSPECT AILERON CONTROL RODS PER IAI S.B. 1124.27-144
DATE COTPLETED
08/L8lO4
l--l llo AerARENT DrscoNTrNUrrrES wERENOTED AT THE TIME OF INSPECTION
f-l lrvsp. nel. ' - /H ;##;" o@- oz/)t6b'22 t/e1a 7I x I NO ATRWOKfHTNESS DE-TERMTNATION
MADE BYTHIS INSPECTION
n u'rsp. REL. FoR MoRETI{ANONE PART OF THE SAME S/N I'NIT.
I SEE A'I-TACHED
-| | see REVERSE
Wallace W. Warren
Page I of 1
FAA CRS XW1R627K
regers fi{:(D,f,, fnc,3418 Cypresswood Dr., Spring, TX77388Office 281 -482-0228 Fax: 281 -355-56 I 5
E-mail: ';t"r l:; i'1r .=. i. \'n r '. . ' ' -...'; :.1'.a' ii''i
INSPE TION REFOXTT & LOGBOOK ATTACHMTIIT
CUST: STARFLITE AVIATION9OOO RANDOLPHHOUSTON, TX 77067
ATTN: Chief Inspeetor
LOCATION: HOU- HOBBY
Item Description:AIRPLANE: WESTWIND 1 124
Description of SlorkPERFORM NDT ONLY I.A.W. THE FOLLOWING: IAI NDT MANUAL PARI 2,27-LO-OO RADIOGRAPHICINSPECT AILERON CONTROL RODS PER IAI S.B. 1124-27-T44
Results:POSSIBLE DISCONTINUITY IN THE FORM OF CORROSION EXISTS IN BOTH VIEWS(LlA/R1A & L1B/R1B) OF BOTH CONTROL RODS.
DATE:8/18/2444WO: SS?S
PO: t{l$S('-$Ft-u4
REG: N83SG
TYPE: I124ASN: 368
TTA: 8605.9
LDGS: 6243
Wallace W. WarrenChief Inspector
Page 1 of 1
FAA CRS XW1R627K
i$tIIi'rN.. I
GENEFIAL OYNAMICS''Aviation Services'
REF. DOCUMENT: Sales OrderPACKING LIST NUMBER: 27 967 57
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04-10-15
2004-1_0-1_5 GARMIN TNTERNATIONAL INC. :Amendment 39-L3645; Docket No. 2003-cE-39-no.
when does this Ro become effective?(a) rnis Ro becomes effective on :u1y 9, ZOO4.
what other ADs are affected by this action?(b) t'tone.
what a'irplanes are affected by this AD?
(c) rhi s AD affects cARMTN Internati onal Inc. GTX 3301330D lvtode Stransponders that are i nstal.l ed oh, but not' l iini ted to, thefollowing airplanes, certificated in any category:
MANUFACTURER
(1) nermacchi S.p.A
(2) neronautica lvtacchi
(3) nerostar Ai rcraftcorporati on
S.P.A
(4) Alexandria Ai rcraft, LLc
(5) Alliance Aircraft GroupLLC
(6) nmerican champion RircraftCorp
(7) Sky rnternational rnc
(8) B-N Group Ltd
(9) eel I anca
(10) gombard'ier rnc
(1-1-) cessna ni rcraft company
s.205-L8/F , s. 205-1_8/R, s. 205-20/R, s . 205-21/ry, s: 208 , s. 2084, F. 260, F. 2608,F.260c, F.260D, F.260E, F.260F, s.211A
AL 60, AL 60-8, AL 60-F5, AL 60-C5, AM-3.
pA-60-600 (nerostar 600), pA-60-601(Rerostar 601-) , pA-60-601-e (eerostar 601p) ,PA-60-602p (Aerostar 602p), pa-60-700p(Aerostar 700P), 360, 400.
L4-L9, L4-L9-2, 14-l_9-3, 1_4-1-9-3A , L7-30,17-31, L7-3LTC, 17-304, 17-3LA, 17-31ATC.
154, 20, H-250, H-295, (USAFU-10D), Ur-295,H391 (USAFYL-Z4), H391B, H-395 (USnrl-2gnor u-10B), H-395A, H-700, H-800, HST-550,HSr-550A (USar AU-24A), 500.
402, 7ccA, 7ccB, 7Kc, 7GCBA, 7ccAA, ZGcBc,7KCAB, 8t<cRg, 8GcBc.
A-1, A-1A, A-1B, S-1S, S-1T, S-2, S-2A,s-2s, s-2c.
BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-2A-6, BN-2a-8, BN-2A-20, BN-2A-21-, BN-2A-26, BN-2A-27, BN-28-20, BN-28-21, BN-2A-26, BN-2A-27,BN-2B-20, BN-2B-21, BN-28-26, BN-28-27,BN-2T, BN-2T-4R, BN-2A MK.rlr, BN2A MK.rlr-2 , BN2A MK. 11_1_-3 .
L4-L3, L4-L3-2. t4-L3-3. 14-1_3-3w.
(otter) DHc-3, DHc-6-1, DHc-6-100, DHc-6-200, DHC-6-300.
L70, L70A, L708, L72, L72A, L728, L72C,L72D, L72E, 172F (USAF T-41A), L72c, L72H,(usnr r041A) , L72r, L72K, L72L, !72M, L72N,L72p, L72Q, I72R, L725, I72RG, pL72D, RL72E(usnr r-41- B) (usar r-4L c AND D), Rl72F(usnp r-4L D) , R1-75c, R172H (usnr r-4LD), RL72J, RI72K, L75, L75A, 1758, L75C,L77, L77A, L778, L77RG, 180, 1804, 1808,l_80c, l_80D, 180E, 180F, l_80c, 180U , 180J ,
l-80K, 182, 1824, 1828, 182c, 182D, L82E,
Page 1
04-10-15
(12) Cirrus oesigncorporati on
(l-3) commander ni rcraftcompany
(l-a) de uar rlland tnc
(15) oynac AerospaceCorporati on
(16) Diamond Rircraftrndust ri es
(L7) Empressa. srasi I ei ra deACTONAUT'I CA S. A. EMBRAER.
(l-8) Extra 11 ugzeugbau cmbh
(1-9) rai rchi I d ni rcraftCorporat'ion
(20) Global Rmphibians, LLc
(21-) crob-werke
(22) Lancai r company
(23) Lanshe Aerospace, LLc
(24) tearjet rnc
(25) t-ockheed Ri rcraftcorporat'i on
182F, 182G, 182H, L82J, 192K, 192L, 192U,182N, 182p, 182Q, l_92R, l-92S, 192T, R192,T182, TRI_82, TL82T, 195, 1954, 1958, l_95C,185D, 185e, A185E, AL85F, 190, (LC-126A, B,c) 195 , 195A, 1958, 2LO, 2104, 2L08, 2i_0c;2l_0D, ZLOE, 2L0F, T210F, 210G, T210G, 210H,T210H, 2L0J, T210J, 210K, T210K, 210L,T21_0L, 210M, T210M, 210N , p210N , T2l-oN,2l-oR, p210R, T210R, 2l-0-5 (205), 2t-0-5A(2054), 206, P2O6, P206A, P206B, P2O6C,P206D, P206E, TP206A, Tp206B, Tp206c,TU206D, TU206E, TU206F, TU206c,206H, T206H,207, 207A, T207, T207A, 208, 2084, 2088,310, 31_04 (USnp U-34), 3108, 310C, 3L0D,31-0E (usAF u-38), 310F, 310G, 3l_oH, E310H,310r , 310J , 310J -1_, E310J , 3l_OK, 3101, 3l_oN ,3l_0p, T310p, 310Q, T310Q, 310R, T310R , 32O,320A, 3208, 320c, 320D, 320E, 320F, 320-L,335, 340, 3404, 336, 337, 3374 (usAr 02e),3378, T3378, 337C, 337e, T337E, T337C,337D, T337D, M337B (USAF 02A), 337F, T337F,T337G, 337c, 337H, p337H, T337H, T337H-sp,401, 4014, 4018, 402, 402A, 4028 , 402C,4LL, 4ILA, 4L4, 4L4A, 42L, 42LA, 42L8, 42LC,425, 404, 406, 441,.
SR2O, SR22.
LL2, LLZTC, L]-ZB, 112TCA, Ll4, LL4A, tL4B,l_14rc.
DHC-2 Mk. r, DHC-z Mk. rr, DHC-2 Mk. rrr.(volaire) l-0, (volaire) 10A, (Rero commander)100, (Rero commander) 1-004, (Aero commander)100-1_80.
DA-20-Al-, DA20-CI_, DA 40.
EMB-110P1, EMB-11OPE.
EA300, EA300L, EA300s, EA300/200, EA-400.
sA26-T, SA26-4T, SA226-T, SA226-4T, 5A226-T(B), 5A227-AT, 5A227-TT, 5A226-TC,sA227-AC (C-26A), 5A227-CC, 5A227-DC (C-268).
colonial c-1, colonial c-2, Lake LA-4, takeLA-4A, Lake LA-4p, Lake LA-4-200, t-ake ptodel2 50.
c1l_5 , G1l-5A, c1l_5B, G115C, Gl_l_5C2 , G1l_5D,G1_1_5D2 , G115EG, G120A.
Lc40- 5 50rc .
MAC-l_25C, MAC-145, MAC-1454, MAC-1_458.
23.
1-8.
Page 2
04-10-15
(26) Luscombe ei rcraftcorporat'ion
(27) tvtaule Aerospace-rechnology, rnc
(28) Mi tsub' sh'i Heavyrndustries. Ltd
(29) uooney Airplane Company,Inc
(30) uoravan a.s
(31) ruavion Aircraft company,Ltd
(32) uew Piper Rircraft, rnc
(33) ostmecklenburgi sche11 ugzeugbau cmgH
(3+; eiaggio Aero rndustriesS.P.A
(35) Pilatus nircraft ltd
1l_A, 11E.
Bee Dee M-4, M-4, M-4C, M-4S, M-4T, M-41_80c,M-4-1805, M-4-180T, t4-4-2L0, M-4-210C, M
-4-2105, M-4-2L0T, M-4-220, M-4 -2205, M
-4-220T, M-5-180C, M-5-200, M-5-210C, M-5-210Tc, M-5-220c, M-5-235c, M-6-180, M-6-235 , M-7 -235 , Mx-7 -235 , MX-7-1_80 , Mx-7-420, MXT-7-1_80, MT-7 -235, M-g-235, MX-7-l_60, MXT-7-1_60, MX-7-1804, MXT-7-1904,MXT-7-1808, M-7 -2358, M-7-235A, M-7-235c,M-7-180c, M-7-260, MT-7-260, M-7-260c, M-7-420AC, MX-7-160C, MX-7-180AC, M-7-420A, MT-7 -420.
MU-28-25, MU-28-35, MU-28-26, MU-28-36, MU-28-26A, MU-28-364, MU-2B-40, MU-2B-60,MU-2B, MU-28-20, MU-2B-20, MU-28-l_5.
M20, M20A, M208, M20C, M20D, M20E, M20F,M20G, M20J, M20K, M20L, M20M, M20R, M20S,M22.
z-242L, z-L43L.
NAVToN , Navi on (L-1-7A) , Navi on (L-l_7B) ,Navi on (L-L7C) , Nav'ion B, Navi on D, Navi onE, Nav'i on F, Nav'i on G, t'lavi on H ,
pA-Lz, pA-12s, pA-18, pA-18s, pA-l_g "l_05"(special), pA-1-8S "1-05" (special), pA-18A,pA-18 "l_25" (nrmy L-21_A), pA-1gS "L25," pA-18AS "L25, " pA-l_8 "l_35" (nrmy L-218) , pA-l-8A "135, " pA-18s "l_35, " pA-18 "l_50, " pA-18A "150, " pA-l-8s "150, " pA-l-8AS "l_50, " pA-1-9 (nrmy L-1_88) , pA-19S, pA-20, pA-20s,pa-20 "l-l-5, " pA-20s "l-l-5, " pA-20 "l_35, " pA-20s "l_35," pA-22, ea-22-L08, pA-22-L35,pA-22s-l-35, pA-22-I50, pA-22s-150, pA-22-160, pA-22s-160, pA-23, pA-z3-160, pA-23-235, pA-23-250, pA-E23-250, pA-24, pA-24-250, pA-24-260, pA-24-400, pA-28-140,pA-28-150, pA-28-151, pA-28-1_60, pA-28-161,pA-28-1-80 , pA-28-235, pA-28s-160, pA-28R-l-80, pA-28s-180, pA-28 -181, pA-28R-200,pA-28R-201, pA-28R-201T, pA-28RT-201, pA-28RT-201T, pA-28 -20LT, pA-28-236, pA-30,pA-39, pA-40, pA-31p, pA-31T, pA-31T1, pA-3LT2, pA-31T3, pA-31-p-350, pA-32-260,pA-32-300, pA-32s-300, pA-32R-300, pA-32RT-300, pA-32RT-300T, pA-32R-301- (sp), pA-32R-301_ (Hp), pA-32R-301T, pA-32 -301,pA-32-301-T, pA-34-200, pA-34-200T, pA-34-220T, pA-42, pA-42-720, pA -42-l_000, pA-42-720R, pA-44-180, pA-44-180T, pA-46-310P, PA-46-350P, PA-46 -500rp.
oMF-100-1_60.
P-180.
PILATUS PC-LZ, PILATUS PC-L7/45, PC-6,
Page 3
04-10-15
(36) Prop-Jets, rnc
(37) Panstwowe zakladvLotni cze (pzt)
(38) PZL wsK/Mielec obrsk
(39) naytheon
(40) nockwell tnternationalcorporati on
(41-) Short Brothers &Harl and ltd
(42) stingsiry Rviation Ltd
(43) socATA-Group Aerospatiale
p!.q H1, pc-6-H2, pc-6/350, pc-6l350-H1, pc-6/350-H2, pc-6/A, pc-6/A-HL, pA-6/A-Hz, pC-6/B--H2, ?C-6/BL-H2, pC-6/82-H2, pC-6/82-H4,PC-6/C-Hz, PC-6/CL-HZ, PC-7 .
200, 2004, 2008, 200C, 200D, 400.
PZL-LO4 WILGA 80, PZL-LO4M WILGA 2OOO, PZL-WARSZAWA, pzL-KoLTBER 150A, pzL-KoLTBER1604.
PZL M2O 03, PZL M26 OL.
35-33, 35-A33, 35-833, 35-c33, 35-c33A, E33,E33A, e33C, r33, F334, F33C, G33, H35, J35,K35, tvt35, N35, p35, 535, v35, v354, v358,36, A36, 436TC, 836TC, 35, A35, A35, C35,D35, E35, F35, G35, 35R, Fgo, 76, 200, 200C,200cr, 200T, A200, s200, B200c, B200cr,B200T, 300, 300LW, 8300, B300C, 1900, 1900C ,l-900D, A100-l_ (U-21J), A200 (C-12A), n200(c-1-2c) , A200c (uc-128) , A200cr (c-l_2D) ,A200Cr (FWC-1_2D), A200Cr (RC-L2D), A200Cr(c-1-2F) , A200Cr (RC-12c) , A200Cr (Rc-1_2H),A200cr (Rc-1-2K) , A200Cr (RC-l_2p) , A200Cr(RC-l_2o , 8200C (C-1_2F) , B200C (UC-12F) ,8200C (uC-1_2M) , 8200c (C-l_zR), l_900C (C-L2J), 65, 465, 465-8200, 65-80, 65-A80, 65-A80-8800, 65-B80, 65-88, 65-R90, 70, 890,c90, c90A, E90, H90, 65-A90-l_, 65-A90-2, 65-A90-3, 65-A90-4, 95, 895, 895A, D95A, Eg5,95-55, 95-A55, 95-855, 95-855A, 95-8558 (T-42A), 95-C55, 95-C55A, D55, D55A, E55,E5 5A, 56TC, A56TC, 58 , 58n, 58P, 58pn, 58TC ,58TCA,99,99A,99A (FACH), A99, A99A, B99,c99, 1-00, 4100 (u-21_F), A100A, A100C, 8100,2000, 3000, 390, 19A, 919, M19A, 23, A23,A23A, 423-1-9 , A23-24 , B23 , C23 , A24, A24R,824R, C24R, 60, n60, 860, 18D, A18A, A18D,s18D. sAl-8A. SA18D, 3N, 3NM, 3TM, IRB-6,D18C, D18S, E18S, RC-45J (SNB-5p), E18S-9700, G18S, H18, C-45G, TC-45G, C-45H, TC-45H, TC-451 , UC-45J (SNB-5) , 50 (r_-23n) ,850 (L-238), C50, D50 (L-23E), D50A, D508,D50C, D50E-5990, E50 (L-23D, nr-23O), F50,c50, H50, J50, 45 (rr-r+), A45 (T-34A or B-45), D45 (r-34B).
Bc-]-A, 4T-6 (sNJ-2), AT-64 (sNl-3), AT-68,AT-6C (SNJ-4), AT-6D (SNJ-s), AT-6F (Srur-6),sNl-7, T-6G, NOMAD Un-260.
SC-7 Series 2, SC-7 Series 3.
T67M260, T67M260-T34.
TB9, TB10, te20, T82L, T8200, TBM 700, M.S.760, M.s. 760 A, M.s. 760 B, na11ye 100s,na1 1ye 150ST, Ra'l 1 ye 150T, na1 1 ye 235E,na11ye 235c, MS 8808, MS 885, MS 8944, MS893a, MS 892A-l-50, MS 892E-l_50, MS 893E, MS894E, GA-7.
AA- 1, AA- 14 , AA- 18 , AA- l-C , AA- 5 , AA- 5A ,AA_58, AG-58.
(44) Tiger A'ircraft ttc
Page 4
04-10-15
(45) rwin commander AircraftCorporati on
(46) un'i va'i r n'i rcraftCorporati on
(47) vul canai r s. p.A
(48) zenai r ltd
500, 500-n, 500-e, 500-u, 500-s, 520, 560,560-n, 560-E, 560F, 680, 680E, 680r, 6g0FL,680F1(P), 680T, 680V, 680W, 681, 695, 690,6904, 6908, 690C, 690D, 695, 695A, 6958,720, 700.
108, 1_09-1, l_09-2, 109-3, l_09-5.
p68, p688, p68c, p68c-Tc, p68 "observer,"P68 "observer 2," p68Tc "observer, "AP68TP300 "Spartacus," Ap68Tp 600 "Viator".cH2000.
what is the unsafe condition presented in this AD?
(d) rhe actions_ specified 'in this AD are intended to prevent interrogatingai rcraft from possibly receiving inaccurate' replies, die t6suppressi on . f rom ai rcraft equi pped wi th the GTX 330/330D tvtode STransponders . when the pu I ses are bel ow the ttti n'imum tri gger Level(url). rhe inaccurate rep'lies could result in vertical se[iration orunsafe TCAS resol uti on adv'i sori es .
what must r do to address this problem?
(e) ro address this problem, you must do the fo1'lowing:
ACTIONS
tnstall crx 330/330D software upgrade to at least version 3.03, 3.04, or3.05.
COMPLIANCE >> >> >>
rnstall the software upgrade within 30 days after :uly 9,2004 (the effective date of this AD), un'less already dohe.
PROCEDURES > >> >>
rol I ow GARMTN tvtandatory Software serv'iceeullet'in No.: 0304, Rev B, dated June 12, 2003(sw versi on 3 .03) ; Garmi n Software Servi cesulletin No. 031-0, Rev A, dated November 10,2003 (sw version 3.04); or Garmin softwareserv'i ce gul I eti n tto. 0401, Rev A, dated rebruary18, 2004 (SW version 3.05).
r request an alternative method of comp'l'iance?
You may request a different method of comp'liance or a differentcompliance time for this AD by following the procedures 'in 1-4 cFR39. 19. Unl ess FAA authori zes otherwi se, send your request toyour principal inspector. rhe principal inspector may add commentsand w'ill send your request to the Manager, wichita ni rcraftcertification office (Aco), FAA. For information on an a1 readyapproved alternative methods of compliance, contact Roger A. souter,FAA, w'itchi ta Aco, 1-801- Ai rport Road , noom l-00, wi chi ta, Kansas 67209;
May
(f)
Page 5
04-10-15
telephone: 31-6-946-4L34; facsimile: 3I6-946-4t07; e -mail address:roger. souter@faa. gov.
ooes this AD 'incorporate any material by reference?
(g) vou must do the actions_ required by this no following the instruct'ionsi n cnRurn ruandatory software servi ce eul l eti n No. : 0304, Rev B, datedJune 12, 2003 (sw version 3.03); Garmin software serv'ice gullet'in No.031-0, Rev A, dated November 10, 2003 (sw Version 3.04); or GarminSoftware Service sulletin No. 0401-, Rev A, dated rebruary 18, 2004(sw version 3.05). _ rhe oirector of the rederal Register approved theincorporation by reference of this service bulletin-in accorijhnce with5 u.s.c. 55?(a) and 1 cFR part 5L. you may get a copy from GARMTNrnternat'i onal rnc. 1200 east l-51-st Street , oi athe , KS 66b62 . you mayrev'iew copies at FAA, central Region, offiie of the Regional counsel,901 tocust, Room 506, Kansas c'ity, tui ssouri 64LO6; or at the offi ce ofthe rederal Register, 800 North capitol street, NW., suite 700,washington, DC.
rssued in Kansas.ci!y, Missouri, on way 13, 2OO4. David R. Showers, ActingManager, smal 1 ni rp'l ane Di rectorate , Ai rcraft certi fi cati on Servi ce.
FOR FURTHER INFORMATION CoNTACT: Roger A. Souter, FAA, wichita Rircraftcerti fi cat'ion offi ce (Aco) , l-801 ni rport Road , Room 100, wi chi ta, Kansas67209i telephone: 3L6-946-4L34; facsimile: 3L6-946-4L07 ; e-mail address:roger. soute'@faa. gov.
Page 6
Westwind 1124Pre and Post Flight inspection
/l-
{ 'Nosti torque link disconnected(n Lav serviced
W Pitot and static covers installed'(' t Gear and tires for condition[cl. E--:-^ -:r r-- -- | - rz'
Post Flight
11.4 F((t>_Engine oit tevets (1 qt tow)/'y'
Signature
Pre Flight
windshields and cabin windows for conditionwings, de-ice boots and stail strip for conditionTip tank fuel valve ctosed (up)Ailerons, flaps and speed brakes for conditionHP rupture membrane in ptaceHyd reservoir levelGear extension cytinder (120A-2000 psi)Thrust reverser cylinder (T10-940 psi)Engines for leaksEngir;g inlets and exhaust for FODExterior ligiftsInterior systems checkedOxygen full (1800-2000 psi)Brake wearTire inflation (nose Sspst main 155 psi)Sumprfuel
Signature
Date f,-t7-o<r
Date 8-r7'o,
Ance..''3h screpa
y.2
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Month-_/ ,/ ,/,/ 4. . 2
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Cert Date
tr,--tt-.t.---e --
It(
Falcon Crest ACcesbories, lni.FAA REPAIR STATION NO, GP2R854K
CUSTOMER: STARFLITE
NOMENCLATURE : WHEEL ASSY
WORK PERFORMED: INSPECT
SERIAL NUMBEH: Dtc xF - 0 33JwoRK oRDER NUMBER: 2 //fO
YES NO TEARDOWN: .
,-Wf DTssAsEMBLE
lL/.1 DISMoUNT TIRE,r'
f lVstatp PArNr & PRTMER-
Lt )rcteAN & |NSPECT WHEEL
V I cLEAN & rNSPEcr BoLTS
./Vryeecr BEARTNGS
/"rr"*wEAR DTMENST.NS
YES NO ASSEMBLY:
r A,ME & REPATNT
Vf MouNr rRE
-tzVI LUBEToRK BoLTS & NUTS
f 4P^IKWHEEL BEARTNGS
f4 BALAN.E *HEEL
stGN^ruRTry?"oerc.: /-rl/-2 \?.\ \'AOO
8318 Branitt Houston, Tx 77061 (713) 644-2290 6oo-e3e-5+zz FAX (713) 644-0356
YES NO NDT INSPECTION:
VT EDDY CURRENT INSPECT WHEEL,/
f / zvalo wHEEL
VT MAGNAFLUX B.LTS
f F ,*srecton
COMMENTS/REMARKS: ,
V4c,/o.,(a ,>r
a
l
l. Approving National AviationAuftority/Country:FAAAJNITED STATES
AUTHORIZED RELEASECERTIFICATE
FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG
3. FormTracking Ref. No.29679
4. Organization: Falcon Crest Accessories, INC. - FAA GP2R854K8318 Braniff Houston. Texas 77061 1-8m-$3-5422
5. Work Order, Confiact, or Invoice Number:w.o#29679
6.ltem 7. Description i 8. Part Number 9.Eligibility"
10. Quantity 11. Serial/Batchnumber
f2. Siaius/work
I WHEELASSY. r 500&150-1 I FEB92-0837 INSPECT
13. Remrks:EDDY CURRENT INSPECTED WIIEEL MAG PARTICLE INSPECTD BOLTS MOIJNTED NEW TIRB PA.{: l84FZ3-2 S/I.{: 41480708-STARFLITE-
i -.
a-yrinqit$sc* rs
-.,1
19.
,V WCFR€.9 Rerurnro Servtcert Other reguladon speclffed in Block 13
Certifies that unless otherwise specified in block 13, the workidentified in Block 12 and described in Block 13 was accomplishedin accordance with Title 14, Code ofFederal Regulations, part 43and in respect to that work, the items are approved to retum toservlce.f"m : 20. Atfhorited Signatriie:
-*^4 t-d$A' 21. ApprovaileetifiCateiNumber:,GP2R854K
lSif{SF{f$ifrirft}ftff 4}
: ',..i : ff..ffizz. Nam{$ryeo or Printed}:
HENRY SANDEFIER
23,Date:07nzDW
User/Installer Responsibilities
It is important to understand that the existence of this document alone does not automatically constitute authority to inshll thepart/componentlassembly. Where the userlinstaller performs worts in accordance with the national regulations of an airworthiness authoritydifferent than the airworthiness authority of the country specified in Block I it is essential that the userfinstaller ensures that his/herairworthiness authority accepts parts/componentVassemblies from the airworthiness authority of the country specified in Block l.Statementsin Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installationcertification issued in accordance with the national regulation by the user/installer before the aircraft may be flown.
-{ Falconr FAA REpAtR STATTON NO. cpzR8s4K
-
E3r6 tsranirf Houston,Tx 77061 (713) 644_2290 it
YES NO TenROOWt't:..
'17VT DISSASEMBLE
Vf DrsMouNr rRE
f 4r^,rpArNr & 'RTMER,r'
-./'l-tu I CLEAN & TNSPECT WHEEL--
W cLEAN { rNSpEcr BoLTS
-
Y trD NU NU I INSPECTION:
f/f EDD' cuRRENr rNSpEcr *HEEL
f /irorowHEEL
VT MAGNAFLUX BoLTS
f I-,nrsrEcro^ %YES NO INSPECTION:
Vf rNSpEcr RAcES
f y'^rrr"r BEARTNGS
.?
f Vcrrc*wEAR DTMENSToNS
YES NO ASSEMBLY:
f QGa,ue& REpArNr
Vf MouNr rRE.?
VT LUBEToRK BoLTS & NUTS
r Arro"^wHEEL BEARTNGS
f /^rr^cE RA6ES
4 BALANoE WHEEL
COMMENTS/REMARKS:
T-<- (/o "n,ilD7
\. ,rVsk-YWl. Approving National AviationAuthority/Country:FAA/LINITM STATES
. AUTHORIZED RETEASE
CERTIFICATEi F4A FoRM gl_90-3r A{rwoIr|tN_ES9 fPPRqyAL rAG
l. Fo'rm rractinlXCf. No.29674
4. Organization: Falcon Crest Accessories, INC. - FAA GP2R854K8318 Braniff Houston. Texas 77061 1-8m-833-5422
5. Work Order, Contract, or Invoice Number:w.o#29674
L Part Number l; 9, l
Eligibility'10. Quantity ii.SeiiatlBatCn
number{2. StaiuClvVo*
WHEELASSY. 5002806-2 I MAR88421 INSPECT
]EDDY CURRENT INSPECTM WHEEL MAG PARTICLE INSPECTM BOL,TS MOUNTED NEW TIRE P/N : 249K83 -3 SA.{:33 I 10787-STARFLITE.
19.
-lv k CFR 43.9 Return to ServiceI-t Cher regulation spedfied in Bloel 13
Certifies that unless otherwise spocified in block 13, the workidentified in Block 12 and described in Block 13 was accomplishedin accordance with Title 14, Code ofFederal Regulations, part 43and in respect to that work, the items are approved to return toservlce.
'f,ryTTT* i 2 t. AppionaVeertifiCatriNumber:
tpzRss+r
flffffifI :;*
22.-Name CrtFed or Printed) :
MARKBERKENMEIER
23.Dite:oTtwnw
User/Installer Responsibilities
It is important to understand that the existence of this document alone does not automatically constitute authority to install theparUcomponenUassembly. Where the user/installer performs works in accordance with the rytio_nal regulations of an airworthiness authoritytlifferent than ttre airworihiness authority of the country specified in Block I it is essential lhat the user/installer ensures that his/herairworthiness authority accepts parts/coinponentVassemblies from the airworthiness authority of the counbry specified in Block l..Statementsin Blocks 14 and 19 db not consrtitute installation certification. In all cases, aircraft maintenance records must contain an installationcertification issued in accordance with ttre national regulation by the user/installer before the aircraft may be flown.
f/
Falcon Crest Accessories. Inc.FAA REPAIR STATION NO. GP2R854K
8318 Branitf Houston, Tx 77061 (713) 644-22g0 TX WATS aoo-sae-scaz FAX (713) 644-0356
CUSTOMER: STARFLITE
NOMENCLATURE: WHEEL ASSY
WORK PERFORMED: INSPECT
PART NUMBen: SOOZ6OO-z
SERIAL NUMBER: MAR88-421
WORK ORDER NUMBER: 29674
YES NO TEARDOWN:.
i- l- orssnsEualr
fr/f DrsMouNr rRE
f F srnrp pArNr & pRTMER
IV I CLEAN & INSPECT WHEEL
IV I CLEAN,& INSPECT BOLTS
YES NO NDT INSPECTION:
fr'f EDDY cuRRENT rNSpEcr wHEEL
f F zycr-o wHEEL
I VI MAGNAFLUX BoLTS
f F ,nsprcron nZNO
rINSPECTION:
INSPECT RACES
INSPECT BEARiNGS
()HECK WEAR DTMENSTONS
rr
YES NO ASSEMBLY:
f I- pnnre & REpArNr
_ -/_l" | , MoUNTT|RE
Yf LUBEToRK BoLTS & NUTS
f F nepncr wHEEL BEARTNGS
f F nrpucE RACES
f f enLANcE wHEEL
coMMENTS/ffEMARKS:' tAu /, j ton 4h,"-{, , 4u^/ Q y'rtn f/a>2 9; *rtt1"'-tN
DArE: 2-7-a7slcNAruRE, fuL<-& U;)ATE' :1 - 4
FORM 639A
UMTEDBATTERIESAI\DAccEssoRIEs'INc.CP,S#U9BNOT8YTT1}BRANIIFFHOUSTON'TX7706I
TEL: 713 991-911 I FAX: 713 991'9117
E-}vIAIL: unitedbatteries@aol'comFORM #9007 -, fv\
NiCad BatterY Pack Work OrO" # " I Cf \ I
curtor., S\1\ML,f € DateReceiv"gl"+ customerY-ryMfg. Tlpe j-I < - g Z: 3 hrntrg. Parr No.Battery PacldCelV
Power SuPPtY Mfg'
SeriatNo. rBt tC
Pre.Service Hiddeu Damage Inspection
General Conditioniec*i"ing Voltage: te"ninrls -f:-Bat,terr ? t^ Zo( % Pack
Receptecle AsrY.
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XNAA,A'TNAFrTu,,:mESLTD I MANUAL
150 HOUR FLIGHT HOURS INSPECTION - MAINTENANCE PRACTICES
NOTE: All items in this section (5-21-00) are to be inspected at 150 hour interuals'
1. Engine
Engine Periodic Inspection. Refer 72-00-00, Inspection / Checksection of applicable AlliedSignal Aerospace Light Maintenance
Manual.
NOTE: For Engine, Nacelle and Pylon Inspection, Refer5-20-07, Maintenance Practices.
2. Starter-Generator
A. Electrical Leads and Cooling Duct - condition and security'
B. Cooling Fan - nicks and blade damage.
C. Brushes Wear Check - Refer 80-10-00, MaintenancePractices and / or Lucas Aerospace Maintenance Manual,File No. 237OO.
3. General
A. Check that a Preflight Inspection has been made.
B. Check all applicable FAA Airworthiness Directivesand Manufacturers'Service Bulletins, Make required logbook entries.
C. Check that all aircraft documents are current and in orderbefore release of aircraft.
LEFT RIGHT
MECH INSP MECH INSP
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FAX RESULTS TO: SEND REPL{CEMENT KIT TO:
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OIL NOW IN USE IS: BRAND. I^4NAIL TYPE:- f1-tl
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REF. DOCUMENT: Sales OrderPACKING LfST NUMBER: 27 52'734
x6510 PAGE: 1DArE: 04/06/04
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FRT TERMS:FOB POINT:
WAYBILL:
SHIP DATE: 04/06/04
CERTIFICATION OF CONFORMANCEits supplis's cenification. rhat the pan ad/or componmts idotified on this shippq m€t the conditions ofthis el6 ofdtr
rh apilicgble specificarions md ile.cogi4qedJg * ii:qtql:T::t ...^^-.-- ^, c.,^nri-r ^di6x rh:ue considqed to be in compliaceu?iri'i"ifii,ild*iJi-'ri,jilui"i,s"1oorSe1tr'srnmufrcrurqorsuppliercenifisthatsuchpartsandcomponfltscomplvwith
productionrequiremmts
I acknowledge tlar I have received the above pans od;or swicc in good conditioo
Sellq furtha cqtifis. or ho on file its suppliq certification, that th6e wffiSello hceby cotifim or ho ondetmined to be inWhse the producion
BY:Signatue
SHIPPED BY:RECEIVED BY:
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1. Approving NationalAviation
Authority/Gountry:
FAA/UNITED STATES
2.
AUTHORIZED RE LEASE CERTI FICATEFAA Form 8130€, AIRWORTHINESS APPROVAL TAG
3. Form TrackingNumber:
w5F385
4. Organization Name and Address:Rockwell Collins lnc.
Collins Avionics Service Center5159 Southridge Parkway
Atlanta, GA 30349(H84R226M)
5. Work Order/GontracUlnvoice Number:
R/E POOL
3. ltem: 7. Description: 3. Part Number: ). Eligibility: 10. Quantity:11. Serial/Batch
Number:12. Status/Work:
1 N ANT60A 1622-2363-001 I N/A | 1 | 174e3 | OVERHAULED
13. Remarks:
Seruiced$-U/-EO S-NJIAS.B.s installed: N/A.CW A.D.: N/A.Tested Per: 523-07661 94-0071 1 I
Refer to attached Service Memorandum (referenced in block 3 above) for service details.Air Data products have been tested and inspected and found to comply with F.A.R. 91-41 1 (Ref Pad 43 App. E).ATC transponders have been tested and inspected and found to comply with F.A.R. 9141 3 (Ref Part 43 App. F)."Certifies that the work specified in block 12113 was carried out in accordance with JAR 145 and with respect to that work theaircraft component is considered ready for release to service under JAA Acceptance Certificate Number: JAA.4333."
14. Gertifies the items identified above were manufacturedin conformity to:-lJ Approved design data and are in a condition for safe
operation -f-'ll-J Non-approved design data specified in Block 13.
rc.Mcrn43.9 Return to Service M.rregulation specified in Block13Certifies that unless otherwise specifled in Block 13, the work identified inBlock 12 and described in Block 13 was accomplished in accordance withTitle 14.Code of Federal Regulations, part 43 and in respect to that work,the itemsare approved for return to service/^
15. Authorized Signature:1 6. Approval/Authorization No.: 2 1 . Approval/Certificate
flo.:
H84R226M
17. Name(TypedorPrinted):
18. Date (m/d/y):-
22. Name (Typed or Printed):
GEORGE T. WARD
23. Date (m/d/y):
10t24t2002
t!sor/l nstal!or Respo !iBibi! itiesIt is important to understand that the existence of this document alone does not automatically constitute authority to install the partcomponent assembly.
Where the user/installer perform work in accordance with the national regulations of an airworthiness authority dlfferent than theairworthiness authority of the country specified ln Block 1, it is essential that the user/installer ensures that his/her airworthinessauthority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.
Statements in Blocks 14 and 19 do not constitute installation certification, In all cases, aircraft maintenance must contain an Installationcertification in accordance wlth the national regulations by the user/installer before the aircraft may be flown.
FAA Form 8130-3 (6-01) *lnstaller must cross-check eligibility with applicable technical data. NSN: 0052-00-012-9005
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2. 3. Form Tracking Number:
AH29404
4. Organizalion Narne ard Address:\
Shoreline dba Safetech8305 Monroe Road Houston, TX 77061
5. Wdk Order/Contracvlnvoice Number
N83SG
6.Itern Descdptkn
7.Pail No
9" Elrsulily' otv
t0.SerhUBatch No
11Statug\ /ork
12.
1. FIRE EXTINGUISHER 327fiXX!4 N/A 1 42129C1 OVERHAULED
13. Remarks
CLEANED & INSPECTED, I.fYDROTESTED iAW D"O.T. EXEMPTION E-7945, OVERHAIJLED, F]LLED, LEAK CI-IECKEO, WEIGHT CHECKED (7.94IbS
INCLUDING CARTRIDGES). PER MFGs CMM 2e2G202 REVISION 2
LAST HYDROTEST:04f04NEXT HYDROTEST DUE: 04/09SPHERE MFG- DATE: 10/80SPHERE EXP. DATE: fiUA
CARTRIDGE LOT# L-12 MFG. DATE: (}9f@ EXP. DATE: 09f6
14. Certifies the iterns ilentified abo\€ vlcre rmnufactured in conformity to:
f] Approvea Oea;ign ffi ard are in a condition for safe operatirxr.
I tton-approreO design data specifir{ in Block 13.
4a z{'w' qZJ 14CFR43.9RelwntoService
I Ottrer regulertion specified in Bbck 13
Certifies that unless otherwise specified in Block 13, the workidentifted in Btock 12 and described in Block 13 was accomplishedin accordance with Title 14, Code of Federal Regulations, part 43and in respeet to that wsr[ the items are approved for return toservice.
1 5. Arithorized Signature: 16. ApprwaUAu{btizdim No W 21 . ApprovaUCertificate No:
wv1R599K
'17. Name (Ty@ or Pdr$ed): 18. Dde( rvdy): d/t{are (Typed or Prir*ed):
J. A" CARMAN
A- Date (rJdly):
04123t2004
Userllnstaller ResponsibilitiesIt is important to understand that the exlstence of thls tlocunrent alone does not automatlcally constitute atrthority to install the
pa rUco m ponenUassembly.
Where the user/installer work in accordance with the national regulations of an Airworthiness Authority different than the Ainrorthiness
Authority of the country specified in block 1 it is essential that the user/installer ensures that his/her Airworthiness Authority accepts
rqrts/components/assemblies from the Airworthiness Authority of the country specified in block 1.
Statements in block 14 and 1g do not constitute installation certification. In all cases aircrafi maintenanc€ records rnust contain an
installation certification issued in accordance with the national regulations by the user/rlnstaller before the aircraft rnay be flown.
FAAForm8130A (64i) * Installenmu$crcschec{<el($billtywihapdicaHetecinbal ffi NSN: ff)5240-012-9005
PARTNUMBER
SERIALNUMBER
D.O.T. SPEC NO.
SHonelme MlRrNe, Inc. dba SnrerecH8305 Monroe
Houston, Texas 770617t3_947_ttt5
_ FAA Repair Station WVlR599kFrn n ExrlNcutsHER WercHr Surrlrraenv
szzpay' CUSTOMER
oz/z?c(€ TfrS-Zrn
I. EMPTY CONTAINER (NAMEPLATE & FILL FITTING ATTACHED)
2. EMPTY CONTAINER (NAMEPLATE & FILL FITTING ATTACHED)WITH CRADLE AND FILL FIXTURE ATTACHED
3. EMPTY CONTAINER WITH FILL FIXUTRE AND FREON SUPPLYHOSE ATTACHED.
DESIRE WEIGHT OF ACENT
DESIRED CHARGED wEIcHT oF CONTAINER (Add line itcm 2 withline item 4)
FILLED CONTAINER (FREON ONLY) WITH cp.ADLE AND FILLFTXTURE ATTACHED (HOSE DISCONNECTED)
CONTATNER VOLUME
W.O. NUMBER
3 .sa
/at(ozLb!'t:
s ?(-8,tl
4.
5.
LBS
LBS
LBS
LBS
LBS
F
PSI
PSI
7. AMBIENTTEMPERATURE
8. BOTTLE PRESSURE DESIRED AFTERNITROGEN CHARGE
9. ACTUAL PRESSURE AFTER NITROCEN CHARGE
IO. FILLED CONTAINER WITH CRADLE AND FILL FIXTUREATTACHED AFTER NITROGEN CHARGE (HOSE DISCONNECTED)
CALCULATED FREON WEIGHT (Subnact line item 2 from line item 6)
CALCULATED NITROGEN WEIGHT (subtrzct line item 6 from lineitem l0)
I 3a. S*Y[\EL, CARTRIDGE, Gff€ibF{EFIGLIJG, SAFETY WIRE,GONESCREEN, INSPECTION TAc &, GzITSKET
I 3b.CARTRIDGE JTJNCTION BOX ASSEMBLYBANJO ASSEMBLY & rNSpEcTroN TAc (GRAVINER)
14. CALCULATED CONTAINER GRoss wElcrn (Add tinc items 1,4, 12,and 13)
15. ACTUAL CONTAINER GROSS WEIGHT
HYDROTEST DATE: o( - z s - o ( WWCHT TAKEN By:
7O"Ooo!:,/f,
640
I l.
t2.
o,[{pl+
il
7, 7/ LBS
-'-_
A-tz
z7d{
&1,,'(, /o t-ss
O, /3 ws
LBS
LBS
wErcHr CERTIFIED nv
/t'*ft&, gerucE p
FORM SS40l 9/29101
- sQUrBwrNo.t#?DATE: o,/+g-ar'
' Shorcline dba Safetech, , Houston Branch - FAA WV1R599K
8305 Monroe RoadHouslon, TX 77061
^ 713-947-1115 71U947-0593 (fax)
Work Order No: AH29404
h Rec'd: 0/,nSl2a04 Date Shipped: / / Date Reqd: o4.n3nA04
Cuetomer: STARFLITE MANAGEMENT GROUP
Account Code: CREDIT CARD-COD
Gust# 895
Customer P.O. # N83SG
Instructions: OVERHAUL-AOG
Part Description: FIRE EXTINGUISHER
Seriaf No: OVI29C1
Qty: 1
Addilional Serial l,lo: 5*359A
MFR: HTL
MFR.#: 327OOO0/.
Teardourn Finding: HYDROTEST DtrE
Corrective Action: CLEAIIED & INSPECTED, HYDROTESTED IAW D.O.T. EXEMPTION E-7945, OVERHAUI-ED, FILLED, LEAK
CHECKED, WEtcHT CHECKED (7.94lbs INCLUDING CARTRIDGES), PER MFG's CMM 26-20-202 REVISION 2
DcscridkmOtv
on&r -atylssue Price
sER-32700004 STD OIFI FOR HTL FIREX ASSY# 327OOOKX &
3270W0l.-1
1 1
INSPECTION CLEAN & INSPECT 1 1
HYDRO.PLUG HYDROTEST PLUG TYPE FIREX 1,|
13004 o-RrhNG - ( MS28775-128 } 2 2
13024 o.RrFrG - (MS2877t021 ) 2 2
13026 o-RrNG ( MS2877t007 ) 1 1
1 3037 O-RING - ( MS;287784') 1 1
13051 GR]NG -(MS29512-10) 2 2
50052-1 ENVIRONMENTAL WARNING DECAL - HALON
AGENTS
1 1
1301 HALON 1301 {CBrF3) (LB")
BROMOTRIFLOUROMETHANE
4.1 4.1
LABOR.PLUG-HTL LABOR FOR PI.UG TYPE IITL F]REX 1 1
AOG ffi*I AC}(? EXPEDITE FEE * 1 1
bareCompleted:04l23n004 Tech: GWDM Inspector: J. A.
THE COMPONENT IDENTIFIED ABOVE IS APPROVED AIRWORTHY WITH RESPECT TO THE WORK
Pana 'l al 4 nttcTrillFp nrtDv
.r-
\rm24 \lul{B,WJit p / MAINTENANaE
EnAa,ffin$rwglszrctm I MANUAL
SCHEDULED MAINTENANCE CHECKS - MAINTENANCE PRACTICES
1. General
A. Prior to commencing inspection, disengage circuit breakers as required to preventdamage to aircraft systems or maintenance personnel.
Record allflight crew complaints and inspection discrepancies on proper paper work.
For Engine Periodic Inspection Requirements, reference Inspec{ion / Check section ofapplicable AlliedSignal Aerospace Light Maintenance.
Remove inspection plates, fairings and covers as required.
Task may be omitted as scheduled maintenance requirement if an equivalent checUtest isperformed as part of the operators flight or ground crew preflight procedures.
Bef91e starting inspections, ensure that protective covering is instalpd over rugs and seatcushions and that all personnel entering aircraft remove siioes or wear wing socks.
B.
c.
D.
E.
F.
Aircraft Orner*i.
.tr /1Serial No. J(oO Registration No. N83$G
Left Ensine Serial *o. ?lt46z Right Engine Serial No.
Aircraftnours 87qt.'3 Landings 6 tr )Left Engine Hours 8 0 / 2- C cycfes S 7V)
Right Engine Hours 7V V V 7- cycles C Al tr
Date fnspection Started 3. Lf:.A < Compteted 4t,aY
? rrq gs
-r;4,L'lrt
5'20-00 ,"i3?Z331
Mu\**ii,fizT,Yljtlp / MAINTENANaE
EnAa. ArcmFrtotlstrrs m I MAIIUAL
NOSE TO FORWARD BULKHEAD - MATNTEMNCE PRACTICES
1. Nose to Forward Bulkhead
A. Jack Aircraft. Refer to 7-1O-OO, Maintenance practices.
NOTE: Before jacking aircraft, deac{ivate the following:
(1) Standby Attitude Gyro.
- For Aircraft 152, 1U, '18't, 187 - 244, 246 and 247 ,
pull out Emergency Power Supply Unit.
- For Aircrafr 245 and 248 - 442, disengage StandbyAttitude Gyro Circuit Breaker, located on FonrrardRelay Box under Copilot Seat.
(2) Pitot and Static Heat - For Aircraft2g' - 442,disengage LH and RH PTTOT STATTC HEAT CircuitBreakers located on Overhead Panel.
(3) Angle of Attack (AOA) Heat - For modet 11244Aircraft only, 295 - 440, disengage AOA CircuitBreaker located on Overhead Panel.
B. Nose Landing Gear.
Refer to 12-1044, Maintenance Practices, Tire Servicingand 3242{0, Removal / lnstallation.
(1) Remove Nose Gear \Mreels - match mark wheel andtire assembly left to right before removal.
(2) Check Tires - wear, weather checking, oil saturation,cuts, flat spots, proper inflation, etc.
(3) Check \Mteels - conosion and damage.
(4) \Mreel Axle.
(a) Check Axle for corrosion (intemal and external),damage and evidence of irregular wear.
(b) Check Axle for cracks using dye penetrantinspection method.
MECH INSP 2S 4oq 800
s/
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X
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ac'2 X
(/
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5-20'01 ,"13?;331
//rt\rulan,Yliflrp / MA1NTENANaE
6EAA AM,FTODI'5'B LN I MANU,AL
Wreel Bearings, Bearing Cups and Spacers.
(1) Remove Bearings - clean and inspect.
(2) Check Bearing, Cups and Spacers for galling.
(3) Pack Bearings. Refer to 12-2O-0O, MaintenancePractices.
(4) Install Nose \Mreels - match marks aligned.
Check following items for general condition, tube integrity,cracks, corrosion, damage, chafing, security of attachmentand leakage:
(1) Check Strut for proper service and correct inflation.Refer to 12-10-04, Maintenanc€ practices.
(2) Outer Strut Body. Perform Penetrant Inspection ofActuating Cylinder Attach Lug Root and UpperBearing Retaining Nut Lock Screw Thread Area.Refer to 32-204'l, Inspection / Check.
(3) Scissors and Bushings - wear (0.020 inch maximumclearance between bushing at knee-joint).
(4) Drag Brac€ Upper and Lower Lugs and Fittings.
(5) Bungee Cables.
c.
(a) Condition.
(b) Dragbrace Downlock Tension Test.Refer to 32-2042,Inspection / Check.
(6) Retract Cylinder and Attach Points.
(7, Inspect Steering Bracket Assemblies for cracks.Refer to 32-50-08, InsDection / Check.
(a) Upper Bracket Assembly (ES12970-7 or2236.0200.000) and Lower Bracket Assembty(ES1 2970€ or 2236.0300.000).
MECH INSP 200 46 800
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t€te ]X
0,)WttilD\ r:"t\- -z rx
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Pre SBVtt\t-24-28 -
vwv-24-28 -1 ,200 hours.
lAtill
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F-c ?X^.-.-*4z\^l<, ./ X
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EFFEGTIVITY: ALL
5-20-0i '":3:''7333
//rt\mna,wJTttp I MA1NTENANaE
EaAa" MmFrcta flB tro I L ANUAL
(b) Upper Bracket Assembly (A0,|-ES1297G.7 or401-2236.0200.000) and Lower BracketAssembly (A01 -ES12970-6 orA01-2236.0300.000).
(8) Trunnion Fittings.
(9) Nose Steering Cylinders and Attach points.
(10) Nose Gear Centering Spring and Attach points.
NOTE: \Mth scissors connected, rotate strut left andright and check for smooth centeringmovement.
(11) Nose Steering Linkage - Universal Joints.
(12) Nose Steering Control Valve.
(13) Nose Steering Control Cables and pulleys.
(a) \Mtile rotating NLG from stop to stop, checkcables for wear, fraying, strand breakage andsecurity, especially at hidden pulley areas.
(b) Check Cable Tension. Minimum tension -19 pounds Refer to 32-5G00, Adjustment /Test.
(c) Pulleys. Inspect for general condition,cleanliness and fee movement.
(d) Cable Inspection. Refer to 32-50-07, lnspection/ Check.
(e) Lubricate Cables. Refer to '12-2O4O,Maintenance Practices.
('14) Gear Uplock Assembty.
(15) Gear Seleclor Valve.
(16) All Hydraulic Lines.
(17) Electrical Bundles, Microswitches, Wring andConnections.
(18) Structure.
(19) Door Actuating Rods and Rod Ends.
EFFECTIVITY: ALL
5-20-01
F.
//rt\;;21E.WI7fl p / MANTENANaE
ENAA. AftNAFTNEI'5IES LTD I MANUAL
(20) Porer Brake Valve and Parking Brake Linkage.
(21) Perform Emergency Hydraulic lndicating SystemHydraulic Fuse Functional Test. Refer to 29-30{6.Adjustment / Test.
Lubricate Gear Assembly and Linkage. Refer to '|2-2O-OO,Maintenance Practices.
Upper and Lower Outer Strut Body Bearings - removerclean, inspect and lubricate. Refer to 32-2041.Removal / Installabon.
Check the following items in and around nosecompartment above nose wheel well for general condition,cracks, conosion, damage, chafing, security of attachmentand leakage:
(1) Pitot Tubes and Lines.
(2) Drain Pitot / Static Drain Valves and Traps. Refer to34-1 0-01, Maintenance Practices.
(3) Electrical Components, \Mre Bundles, Wndshield
Ale.r Dr"re
t l- 06..JY
8?r z.r
Ne"r U,rtl octo
(6)
(7)
(4)
(5)
(1)
(2)
Heat Resistors and Terminal Strios.
All Structure
Orygen Lines and Bottle(Refer to 5-10-00,)Maintenance Practices. ---"-------------l
Avionics Components and Shock Mounts.
AC Inverters (forward or aft installation) and CoolingFan.
For aircraft equipped with Collins WXR-300 WeatherRadar - check Crystal Desiccant Bottle. Refer to34-40-04, Adjustment / Test, Paragraph F, Desiccant
(8)
H.
Check.
Radome
Condition and security.
Static Discharge Diverter Strip Bonding. Refer to23-60-00, lnspection / Check.
\-/
$jtf 2@ ,tOO 800
u[ ac-2 X
Vo.A
1,200 hoursor 3 years,whicheveroccurs first
,rYl| ,(u
\oc- ),
N/o1 ,200 hoursor 2 years,whicheveroccurs first
t
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//rr\*ill1H,Vlifllp / MAtNrENArycE
Exlra. ArcaAFrrva.rlrg tm / MANUAL.^
MAINTENANCE PRACTICES
1. Fuselaoe - Forward Pressure Bulkhead to Aft pressureBulkhead
A. Instrument Panel - Check general condition:
(1) Accessible Instruments, Hoses and Lines.
(2) Accessible Electrical Wire Bundles and Connections.
B. Pressurization System - Check:
(1) Accessible Hoses and Lines - condition.
(2) lsobaric Valve safety wired in open position.
(3) Clean Cabin Air Pressure Controller Air Filter. Referto 21-30{1, Cleaning / Painting.
(4) Replace Air Filter Element Cartridges.
Oxygen System - Check:
(1) Crew Oxygen Masks.
- For aircraft with EROS Mask and RegulatorAssembly, refer to 35-00-00, Adjustment / Test,Paragraph 2A and 2B..
- For aircraft with Puritan Bennett Mask andRegulator, ref. 35-00-00, Adjustment / Test,Paragraph 2A.
(2) Passenger Oxygen Supply System Test - Referto 35-0G00, Adjustment / Test.
\A/indshield, V\f ndows and Pilot Openabte \A/indow.
(1) Delamination, scratches, cracks, seal and latch.
c.
D,
Page 2O1Jan 31/2003
MECH INSP 240 4@ 800
sta:i
'#)
Yf/" xi /y
j/8;,/p, I
\X
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\ or 1 year,I whichever,/ occurs first
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EFFECTIVITY: ALL
5-20-02
u,r\ulln.Ytitm I MATNTENANaE
EnAE ArcnAFTrtM.atE LrD I futANUAL
(2) Renew or reactivate desiccant crystals as necessary.lf moisture is noted between window panes, performprocedure to remove residual moisture. Refer to3040-00, Maintenance Practices, Service DesiccantSystem.
CAUTION: DO NOT EXCEED 2.0 PSl.
(3) Terminal Contact Assemblies for arcing.
(4) Check Pilot and Copilot Side Wndows for cracks inflange, radius of flange and around all attachmentfasteners. Refer to 56-10-03 and 56-10-04,Inspection / Check.
NOTE: Not applicable to Cockpit Side \A/tndow(34301 7-507) (pilot) or (343003-501 )(copilot), post Service Bulletin 1 124-56-1 1 3.
(5) Wndshield \ /iper Assembly - condition and security.Refer to 3G.40-00, Maintenance Practices.
Control Pedestal - general condition.
(1) Indicators.
(2) Controls.
(3) Switches.
(4\ Electrical connections.
(5) Throttles and Piggy Back Levers - ease of operation.
Overhead Elec-trical Panels - general condition.
(1) Electrical bundles, connections, damage andtightness.
CAUTION: ENSURE ADEQUATE CLEARANCEBET\ ,EEN ELECTRICAL CONNECTIONSAND FMME W{EN INSTALLING PANEL.
ATC Transponder Test and Inspection.Refer to FAR 91 .413.
Altimeter Systems Tests and Inspections.Refer to FAR 91.41 1.
F.
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EAA€ ATNAF| ,/a,/sI'€S LN I MANUAI
Check operation of Fire Protection System. Refer to26-00-00, Maintenance Practices, Paragraph 1,A or 18.
Battery Temperature System - perform Functional Test ofBattery Temperature and Waming System. Refer to24 -3041, Maintenance Practices.
Check all Internal and Extemal Lights including Cockpit'Press-to-Test' Lights.
Remove covers from the following listed electrical boxesand check inside for cleanliness, safety and condition ofelectrical parts.
(1) Forward Relay Box (belo\,\, copilot seat).
(2) Fire Control Box (betow pilot seat).
Seats, Mountings and Seat Belts - Condition.
(1) Pilot.
(2) Copilot.
Rudder Pedals, Linkage and Bellcrank.
(1) Brake Valve Linkages.
(2) Freedom of operation.
Cabin Entrance Door. Ref. S2-10-OO, Insoection/Check.
(1) Ease of operation.
(2) Door Hinges.
(3) Locking Mechanism.
(4) Door Seal condition.
(5) Clean and lubricate Door Seals - silicone lubricantrecommended.
NOTE: Apply only a very light coat of lubricant;excessive lubricant will collect dirt and causedoor seal leakage.
(6) Lubricate - Refer to 12-2OeO, MaintenancePractices.
T/lEAU Dt( 2m 6 800
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EFFECTIVITY: ALL
5-2A-02 .,"I:?;333
//u\lnl1n,rcIlxm I MATNTENANaE
E 'dlAATRAFr
feifilEsl7E- I MANI'AL
P.
(7) Door step - condition, operation and presence ofsroppers.
Passenger compartment - general condition and security.
(1) Emergency light - check operation, security,cleanliness and connections. Check battery charge.Refer to 12-10-06, Maintenance Practices.Paragraph 3.
NOTE: Every 200 hours or not to exceed 3 monthsor whenever the emergency lights have beenoperated from the emergency battery formore than 'l hour.
(2) Refreshment bar, ice chest, galley coat closet,cabinets, tables, etc. for ease of operation andlocking.
(3) Seats and Seat Belts.
(4) Oxygen, Reading Light, and Ventitating Air Consote.
(5) \Mndows - delamination, scratches and cracks.
(6) Interior lights.
(7) Emergency Exit.
(a) Check Release Mechanism. (Pull releasehandle, but not necessary to remove exit fromaircraff.)
(b) Remove Exit - inspecl seal and check operationof game tables for clearance.
(8) Certificates.
(9) Avionics components - security and connections.
(10) Lavatory and Baggage Compartment - condition.
(1 1) Lavatory Door- operation.
(12) Check Portable Fire Extinguisher. Referto 5-10-00,Maintenance Practices.
MECH INSP & 1t 800
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//u\L;ltzlE,Elt p / MATNTENANCE
Enr'.g,. ArcRAFTNA.FIES LM I MANUAL
O. Flight and Passenger Compartment:
(1) Remove Flight and Cabin Compartment Seats,Divan, Seat Tracks and carpet as necessary to gainaccess to floor paneling. Thoroughly inspect underfloor for corrosion, damage, wear, security,cleanliness and ensure that all under floor drain Dathsare clear of debris and sealant.
(2) Flight Control System - Pulleys, Brackets, Guaros,Bellcranks and Push-pull Rods - condition, operationand security of attachment.
(3) Control Column Interconnect Cable.
(a) Condition and security. Refer to 27{0{0,Inspection / Check.
(b) Check Cable Tension. Refer to 27-00-00,Maintenance Practices. Table 2.
(4) Flight Control Transition Cables between FuselageStation 153 and Station 269.
(a) Condition and security. Refer to 27-0000,Inspection / Check.
(b) Check cable tension. Refer to 2740-00,Maintenance Practices, Table 2.
(5) Lubricate Control System. Refer to 12-2O-OO,Maintenance Practices.
(6) Lubricate Gustlock Mechanism. Refer to 12-20-00,Maintenance Practices.
(7) Perform Aileron and Rudder Static Friction Test.Refer to 2740-00, Maintenance Prac'tices.
(8) Engine Control Linkage and Teteffex Cable -condition, proper routing and security of clamps.
(9) Plumbing - proper routing, chafing, tube integrity,condition and leaks.
(10) Check general condition and security ofPressurization and Air Conditioning Componentsunder cabin floor.
EFFECTIVITY: ALL
-20-02 .,"13?;333
//rt\ln2an,wjrttp / MA|NTENANaE
EeaaArcmFrrwlelg Lro I IWANUAL
(1 1) Inspecl Structure under floor below galley andlavatory toilet installation for fluid leakage, corrosion,general mndition and cleanliness.
Standby Attitude Gyro - Check Standby Attitude GyroEmergency Power Supply Unit condition every 20d hoursor not to exceed 3 months or whenever the standbyattitude gyro has been operated from the emergencypower supply for more than 45 minutes. Refer to 34_20_09.
n5,,^.a, I
5)uAdjustment / Test, Paragraph 2A.
Check the following for condition:
\A/lndshield \Mpers.
(1) Oxygen Thermat Discharge Disc.
(2, Fuselage Skin.
(3) Cabin Outflow and Safety Valves - condition andcleanliness.
(4) Static Sources.
(5) Drain Pitot and Static Valves and Traps.Refer to 34-10-01 , Maintenance practices.
(6) All Drain Holes and Accessible Fiftings.
(7) Antennas - condition.
(8) Accessible Electrical Connections and Components -damage, tightness, chafing, fraying and cuts.
(9) Accessible Electrical Connections and Comoonents ldamage, tightness, chafing, fraying and cuts.
EFFECTIVITY: ALL
5'20'.OZ ,"f3?;3S
//rr\*u2oE,W.rntm / MATNTENANaE
6RAa. ArcnffrrtptlsltFEsmo I MANUAL
WNG - MAINTENANCE PRACTICES
(a)
(b)
(c)
"4
1. \Afing
A. \Mng Flap - general condition, security andcracks.
(1) Skin and Rivets.
(2) Attach Points:
Inspect Hinges and Bearings.Refer to 27-50-00, Inspection ICheck, Paragraph 24.
Inspection Hinges and Bearings.Refer to 27-5040, Inspection /Check, Paragraph 28., Steps (2),(3) and (a).
Bonding Jumpers.
! Condition, fraying andsecurity.
2 Control Surface Bonding.2360-00, Inspection/Check.
(3) Flexible Drive Shafts.
(a) Couple Nuts - security, routing,freeplay and structure
(b) Clean, inspect and lubricate.Refer to 27-50-00, Servicing.
Actuating Jacks - attach points,electrical connec{ions, rigging andmicroswitch sliders.
Flap Position TransmitterPotentiometer - attach pointsand electrical connection.
Netr Dr
3?s o(4)
(5)
EFFECTIVITY: ALL
5-20-03 ,"i3?;331
//rt\ilr4E.YJ?ttp / MAINTENANaE
ANAA,,|FF/,FTNa'''INE LN / MANUAL
(6)
(7)
Check Flap Vane Segments -condition, failed or loose fasteners andsecurity of aftach plate. Ref. 27-50-00,Inspection/Check, para. 1. C.
Check Flap Vane Segments -separation of skin from honeycomb.
(a) Visually inspect upper and lowersurfaces for local bulging orlooseness of skin.
(b) Tap test by lightly tapping theskin with a coin or equivalent andcomparing the sound at adjacentlocations. Separation betweenskin and honeycomb core canreadily be identified by a hollowsound compared to theat solidly bonded areas. Ref.27-50-00, I nspection/Check,para. B. (2), (3).
Flap System Time-Exceed Relay Check.
(1)
(2)
Move Flaps to '12' or 20' position.
Open Flap Control Circuit Breaker onOverhead Panel. Disconnect FlapMotor Plug P-26.
Close Flap Position Indicator and FlapControl Circuit Breakers on OverheadPanel and Flap Circuit Breaker(CB2-5) on No. 2 DC Contactor Box.
Activate Flap Selector to DO\ANDosition.
(a) On aircraft with a 14 Flap ControlCB - Breaker should trip after2Oj3 seconds. ReDeatprocedure in UP position.
(3)
(4)
'-r'\\
//rr\
(5) Check Flap Vane Segments -condition, failed or loose fasteners andsecurity of attach plate. Ref. 27-5040,Inspection/Check, para. 1.C.
(6) Check Flap Vane Segments -separation of skin ftom honeycomb.
(a) Visually inspect upper and lowersurfaces for local bulging orlooseness of skin.
(b) Tap test by lightly tapping theskin with a coin or equivalent andcompadng the sound at adjacentlocations. Separation betweenskin and honeycomb core canreadily be identified by a hollowsound @mpared to the responseat solidly bonded areas. Ref.27-50-00, Inspection/Check,para. B. (2), (3).
Flap System Time-Exceed Retay Check.
(1) Move Flaps to 12' or 20' position.
Open Flap Control Circuit Breaker onOverhead Panel. Disconnect FlapMotor Plug P-26.
Close Flap Position Indicator and FlapControl Circuit Breakers on OverheadPanel and Flap Circuit Breaker(CB2-5) on No. 2 DC Contactor Box.
Activate Flap Selector to DO\MI|Dosition.
(a) On aircraft with a 1,A FlaD ConholCB - Breaker should trip afier2013 seconds. Repeatprocedure in UP position.
r'fi/C)7q**
(2)
(3)
(4)
EFFECTIVIW: ALL
5'20-03 .,"I3?ir333
D.
//u\nnlln,Ytitlp / MAINTENANaE
BEAA.
(5) Push-Pull Tube.
(a) Inspecl extemal surface of Tubefor wear (particularly area ofrollers). Maximum reduction oftube crosswise diameter is0.012". Ref. FAA AirworthinessDirective No. 96-24-1 1.
(b) Clean all Guide Rollers andcheck Rollers for smoothrotation.
(6) Lubricate Trim Tab and Servo TabHinges ftom inside with LPS-3 orequivalent.
(7) Aileron Bellcrank - check Travel Stopsmake coniact in both directions of fulltravel - attach points and safety.
(8) Check Aileron Control System Trimand Servo Tabs for free-play.Refer 27-10-00, lnspection / Check.
(9) Static Discharger Wcks and Bases.
(a) Condition and security.
(b) Static \Mck lnspection / Check.2360-00, Inspection / Check.
(c) Wck Base Bonding Inspection/Check. Refer 23€G00,Inspec'tion / Check.
Non-lcing Fuel Vent - obstruction and fuelleakage.
Tip Tank.
(1) Tip Tank and \Mng Fillet - condition,security and fuel leaks.
LEFT RIGHT
MECH INSP MECH INSP ffi lry e00
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EFFECTIVITY: ALL
5'20-03 ,,"i3?;33i
\r/ -
//u\ia-21rE,Wlitlp / MAWTENANaE
EnAa.ArcaAFrfiig,lstn tm I MANUAI
.'',^,
(2) Vortex Generators - security ofattachment and / or missingGenerators. Refer 57-20-01.
(3) Navigation Light Lens (Position andStrobe) - condition and security.
(4) Landing Light - condition and security.
(5) Drain holes - cleanliness.
(6) Static Discharge Wcks and Bases"
(a) Condition and security.
(b) Static \Mck Inspection / Check.23€0-00, Inspection / Check.
(c) \Mck Base Bonding Inspection /Check. Refer 23€G00,Inspection / Check.
(7) Tip Tank Tail Cone Diverter StripBonding Inspection / Check. Refer23€0-00, Inspeclion / Check.
Wng Skin - condition and fuel leakage.
Fuel Tank Drains - leakage.
Wng Skin Fairing - cracks and loose rivets.
All Plumbing attached along wing rear sparfor proper routing, chafing, tube integrity,condition, security and leaks.
NOTE: Check for clearance between fluidlines and flap flex drive cables andaileron torque tubes while flaps andailerons are moved through fulltravel.
Speed Brakes and Lift Dumpers - condition,security, hydraulic leakage and microswitch(Ri/H outboard only).
F,
G.
H,
t.
J,
EFFECTIVITY: ALL
5-20-03 ,"I3ffi33
//rr\i;i21 iT,}ETJIID / MA IN TENA NCE
,sruarrrzuTnnaTrlEs tm I MANUAL
\A/ire Bundles entering Wng from AfiFuselage - damage and security.
Check Fuel Dump System:
(1) Functional Check - Fuel DumpSystem. Refer 28{0-00, MaintenancePractices, Fuel System OperationalCheck, Paragraph 4.8.
(2) Check Fuel Dump System foroperation only (without measuringtime/quantity). Refer 28-00{0,Maintenance Practices, Fuel SystemOperational Check.
Leading Edge and Pneumatic Deicer Boots -check condition.
lle*rDrs
1,lgg.r
Pase2o6 /-
LEFT RIGHT
MECH INSP MECH INSP E 4i 800
& (nttQc )r 6{i lx
,lo
7
1,200 hours
r.ttp NIA,
X
/ I * X
EFFECTIVITY: ALL
5-20-03 Jan 31/2003
//rr\!;iz1a.Hittp / MA1NTENANaE
ANAET 4#HAF7'V4,TS?E L7D I MANUAL
MAIN LANDING GEAR - MAINTENANCE PRACTICES
1. Main Landing Gear
NOTE: Steps 1.A. thru 1.D. may be performed attire change but not to exceed 200 hourintervals.
A. Remove Main Gear \Mteels.
Refer 12-10-M, Maintenance Practices, TireServicing and 32-4't -00, Removal /Installation.
(1) Tire - wear, weather checking,oil saturation, cuts, flat spots, properinflation, etc.
(2) \Meel - corrosion, damage, overheatindication and wheel half retaining boltlooseness,
(3) Drive Keys - looseness and wear.
(4) Blow-Out Ptugs - damage andleakage_
(5) \Mleel Axle.
(a) Check Axles for conosion(internal and external), damageand evidence of irregular wear.
(b) Check exposed area for cracks -use ctye penetrant inspectionmethod.
LEFT RIGHT
MECH INSP MECH INSP a 6 800
afi
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EFFECTIVIW: ALL
5-20-04 ,"13?;333
azzc\;;4/E,YliXrp / MA1NTENANaE
Ema. ArcaAFrcra.omatm I MANUAL
(6) Anti-Skid Detectors - remove, checkfor conosion and contamination. Cleanas required and coat axle interiorsurface with Dow Corning 4 compound(MlL-S€6608, Amendment 3). Instail.Refer 3244-06, Removal /
\/wteel Bearing, Bearing Cup and Spacer.
(1) Remove, clean and inspect Bearing.
(2) Inspect Cup for galling and spalling.
(3) Pack Bearings. Refer 12-20-00,Maintenance Practices.
Brake Assembly.
(1) Brake Mounting Flange - cracks.
(2) Brake Disc - cracks and maximumwear.
(3) Brake Housing - leakage.
(4) Brake Lines - chafing, frayedand leakage.
Installation.
(1) Install main gear wheels.
(2) Check security of drive clip and cap.Check Clip gap is 0.140" i0.010,'.
(3) Anti-Skid System - check.
Anti-Skid Control Switch - OFF(both Anti-Skid INOP Lights ON)
Anti-Skid Control Switch - ON(both Anti-Skid INOP LightsOUT)
D.
(a)
(b)
VEFFECTIVITY: ALL
5'20-04 ,"I:?;333
u/r\ill1H,YJitm / MATNTENANaE
EAAaANAE| /g/s'rc UD I MANUAI.->.
. (7)
(8)
(e)
(10)
Main Landing Gear - check for generalcondition, cracks, security of attachment andleakage.
(1) Strut - check for proper service andcorrect inflation. Refer 12-1044,Maintenance practices. tr f-l ( j.
(2) Upper Body.
(3) Fork.
(4) Scissors.
(5) Side Brace, Lugs and Fittings.
(6) Retract Cylinders and AttachingPoints.
Jury Brace.
Trunnion Retaining Bolts - tightness.
Microswitches,
Electrical Connections and \AtlreHamesses.
I
(11) Sealing Compound around Main\Meel Axle Plug Button Grommet andAnti-Skid Conduit upper flared end.
F. \Mreel Well - check for general conditionand security.
(1) Uplock Assembly - leakage.
(2) All Fluid Carrying Lines - chafing,damage, tube integrity and leakage.
(3) Electrical Connections and WreBundles.
(4) Structure - Paint condition andcorrosion.
(5) Main Gear Doors and Linkage.
LEFT RIGHT
MECH INSP MECH INSP 2€' 4{n 800
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EFFECTIVITY: ALL
5'.20-04 ,"13?;333
/rr\uifi tT,tETtlD / MAIIv|TENANaE
rsaAa gftaAFrnlr,s.ns tm I MANUAL
(6) Fuel Vent Lines and ClamDs.
(7) Microswitches - Uplock and Downlock.
Lubricate Gear Assembly and Linkages.Refer 1 2-20-00, Maintenance practices.
H.
(1) Remove upper and lower ActuatorAttach Bolts and lubricate. Refer12-2O-0O, Maintenance practices.
Landing Gear - Funclional Tests.
(1) Normal System. Refer 32-30-00,Adjustment / Test.
(2) Free Fall Extension. Refer32-30-00,AdjustmenUTest, Normal SystemFunctional Test.
(3) Emergency Gear Extension ControlCable. Refer 32-3040, Adjustment /Test.
(4) Emergency Extension System. Refer32-30-00, Adjustment / Test.
Perform Anti-Skid System Functional Test.Refer 32-4440, Adjustment / Test.
Standby Attitude Gyro - before loweringaircrafr from jacks, activate and checkoperation of Gyro:
- ForAircraft 152, 154, 181,187 -244,246and 247 , install Emergency Power SupplyUnit.
- For Aircraft 245, 248 - 442, engageStandby Attitude Gyro Circuit Breakerlocated on the Foruvard Relay Box underCopilot Seat.
LEFT RIGHT
MECH t,ryFRKtrun llgF .(il { 800
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*7>\
'-ln X
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EFFECTIVITY: ALL
5-20-04 *f3ffi3i
u,4\urnn,vlttB I MA1NTENANaE
F'EAAArcEAFTT,PIA"E LM I MANUAL--7\
Lower Aircraff offjacks. Refer 7-10-00,Maintenance Practices.
NOTE: Ensure all other services andinspection checks reouired withaircraft on jacks are completedbefore aircrafi jacks are lowered.
NOTE: After lowering aircraft from jacks,reactivate the items listed below:
(1) Pitot and static heat for Aircraft295 - 442, engage LH and RH PTTOTSTATIC HEAT Circuit Breakerslocated on Overhead Panel.
(2) Angle of Attack (AOA) Heat - Formodel 1 1244Aircraft only, 295 - 442,engage AOA Circuit Breaker locatedon Overhead Panel.
LEFT RIGHT
MECH INSP MECH INSP aa & 800
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EFFECTIVIfi: ALL
5'20-04 .,"13|2333
...>\
//u\ilrAE,Vlttp / MA1NTENANaE
EAAS,.ArcAAFT{IfrXA''IE UO I MANUAL
AFT FUSETAGE - MAINTENANCE PRACTICES
1. Afi Fuselaoe (Station 270.00 to Station 452.00)
A. Flight Control System - Aileron, Elevator and Rudder.
(1) Transition Cable Bellcranks.
(a) Cable Swages - locked in place.
(b) Torque Transfer Tube - attach points.
(c) Flight Controt Cables - condition.Refer to 27-00-00, Inspection / Check.
(2) Aileron, Elevator and Rudder Torque Transfer T
(a) Attach Points.
(b) Freeness of Bearings.
(c) Safety.
(d) Autopilot Servos - security.
(e) Lubricate Control System.Refer to 12-2OeO, Maintenance practices.
(f) Control Cables and Air Pressure Seals atStsation 269 - condition and security. Lubricatecables and seals. Refer to ZZ-OO0O,Maintenance practices, para. 4.
(3) Flap Prime Mover and Flex Shafts - generalcondition, security,
B. Above \A/ing Aft of Station 316.
(1) ElectricalBundles.
(2) Structure.
C. Electrical System Components AC and DC:
(1) Security in Mounting.
(2) Wre Bundles - damage and security.
-
MECH INSP 2C 106 800
;4 X
z/ X
,H X
-h' X
Az X
_v X
Jl X
At /t X
lt/A X
-8y X
K9 X
Jr) X
-P X
22 X
EFFECTIVITY: ALL
5-20-05 ,"13?,?331
//rt\;i2'E,Yliflrp I MA1NTENANaE
BaAE ArcaAFr Na,.clg ED I MANaIAL
(3) Batteries.
(a) Remove from aircraft for servicing andcharging. Refer to 12-10-c€, MaintenancePractices.
(b) Check for any evidence of corosion or physicaldamage.
(c) Check Vent Lines - obstruction and security ofinstallation.
(d) Check Quick Disconnects - corrosion andgeneral condition.
(4) Remove covers from the following listed electricalboxes and check inside for cleanliness, safety,condition and evidence of overheating of electricalpans.
(a) DC Contac{or Boxes, Left and Right.
(b) Flap Contactor Box.
(c) Afi Relay Panel.
(d) Horizontal Stabilizer Actuator Relay Box.
(e) AC Inverter Blower Control Box.
(5) Perform voltage check across Wndshield CyclingContactors (\AEC). Refer to 30-40-00, MaintenancePractices, Paragraph 1.B.
(6) Perform resistance check of Circuit Breakers CB1-4(Left DC Contactor Box) and CB2-4 (Right DCContractor Box). Refer to 24-50-00, Inspec{ion /Check.
(7) Perform Distribution Bus Circuit Breaker Inspection.Refer to 24-5040, Inspection / Check.
(8) Perfa[F-] Inspection and Test of Priority Bus Diodes.Refer to 24-5O4O,Inspection / Check.
D. Speed Brakes and Lift Dump System - performOperational Check. Refer to 27€0-00, Adjustment / Test.
MECH INSP 2@ 4m 800
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EFFECTIVIW: ALL
5-20-05 .,"13?;333
//24 \-..ruzaB.Yljttp / MA1N|ENANaE
RaAa,ArcnAFrerotlg E tm I MANUAL
Landing Gear Emergency Extension System.
(1) Landing Gear Emergency Extension Systempressure. Refer to 12-1O44, Maintenance practices.
(2) Nitrogen Bottle - annual visual inspection andperiodic hydrostatic. Refer to S-10-00, MaintenancePractices and 32-30{0, lnspection / Check.
Throftle Cable (Teleflex) Push-Pull Power Control.
(1) Fraying.
(2) Safety.
Fuselage Fuel Tank Area - general condition and leakage
(1) Fuel Shutoff Valve. Cycle OFF and ON.
(2) Fuel Supply Line - condition.
(3) Fuel Boost Pump Area and Pressure Refueling pointArea.
(4) Check Operation of Fuel Boost Pumps, pressureSwitches and Automatic Changeover. Refer to28-00-00, Maintenance Practices - Fuel SystemOperational Check, Paragraph 4.F.
Air Conditioning and Pressurization Equipment.
(1) Change Cooling Turbine Unit Oil.Refer to 12-10-1O, Maintenance practices.
Ducting and Tubing - security and condition.
Clamps - security and condition.
\A/ater Separator - cleanliness and condition.Refer to 21-7O-O1, Inspection / Check.
(a) Clean or replace Cloth Condenser.
(b) Clean \Ahter Drain Filter.
Check operation of all Valves and Switches.Refer to 21-20-00, Adjustment / Test.
E.
F.
G.
(2)
(3)
(4)
(5)
MECH INSP N d 800
-'H X
-L/ X
/r X
'(lD XI
(t,DY x,AD
X
ltt X
llt)r x
s2 X
w X
M X
J/ X
,* X
.D x
EFFECTIVITY: ALL
5-20-05 ,"13?;333
//rt\[n21n,H7t p / MA|NTENANaE
|s'd,A, ArcNAFr$/,'rflNf5 LN I TNANUAL
t.
(6) Perform Bleed Duct Overpressure Switch Check.Refer to 21-60-10,Inspection / Check.
(7) 35 Degree Duct Sensor - inspect ElectricalConnection for corrosion. Clean Electrical Connectorand Sensor with Non-CFC Dry Type ElectricalCleaning Spray. Pack Electrical Connector with DC-4(Dow-Coming) Compound.
(8) Bleed Switching Valves - visually inspect.
(9) Refrigeration Unit Mounts - condition and security.
Hydraulic System Components - Aft Fuselage.
(1) Fluid Carrying Lines and Fittings - teakage, tubeintegrity, chafing and security.
NOTE: Check for clearance between Fluid Lines,Flap Flex Drive Shafts and Aileron TorqueTubes while Flaps and Ailerons are movedthrough full travel.
(2) Lift Dumper and Speed Brake Selector Valves -leakage and electrical connections.
(3) Hydraulic Power Panel - leakage.
(4) Hydraulic Emergency Brakes Accumulator DryNitrogen Charge. Refer to 12-10-03, MaintenancePractices.
(5) Thrust Reverser Accumulator
(a) Thrust Reverser Accumulator and Cylinder DryNihogen Charge, Referto 12-10-03,Maintenance Practices.
(b) Nitrogen Bottle - annual visual inspection andhydrostatic test. Refer to 5- t 0-00, MaintenancePractices and 78-34{0, MaintenancePractices, Gas Storage, Bottle, Paragraph 4.
(6) Hydraulic High Pressure Filters - check red pop-outbutton. lf button is out (extended), Filter is clogged;Filter Element must be replaced and applicable pumpchecked.
MECH INSP 2# 4fr 800
A)k X
_z/ X
//J) X
U' X
i/nl/j.) X
,'lllV' k'
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EFFECTIVITY: ALL
5'20'05 t.i?l',irl?
//rt\L;i;21A'W7Xrp / MA1NTENANaE
ENAE ArcMFI TIDI,sIES LTD I MANUAL
(8)
(e)
(7) Replace Hydraulic High Pressure Filters andReservoir Filter,
Hydraulic Reservoir Air Pressure Filter - clean. Referto 29-10-00, Removal / Installation, Paragraph 4.
Hydraulic Reservoir Air Vent Filter - replace. Refer to29-10-00, Removal / Installation, Paragraph 6.
(10) Clean Hydraulic Reservoir Air Pressure CheckValves (4 each) - Check Hydraulic Reservoir forPressurization. Refer to 29-1040, Removal /Installation, Paragraph 3.
(1 1) Anti-Skid Control Valves.
(a) Leakage and electrical connections.
(b) Clean Filters. 3244-02,Inspection / Check.
Pylon - Engine Mount Beams attach points.
Hoses, Lines, Electrical Bundles entering Fuselage fromEngine Nacelles - condition, damage, chafing, tubeintegrity, leaks and security.
Fire Extinguisher Containers - security, eleetricalconnections, nitrogen pressure. Ref. 5-1040, MaintenancePractices, Container and Cartridges.
Electrical Bundles and Terminal Strips - damage, securityand loose connections.
Pneumatic Deicing Equipment.
(1)
(2)
(3)
(4)
Security and condition.
Electrical connections.
Air Ejector - clear.
Remove and inspect Deicer Check Valves located attee, upstream of Pressure Regulator Valve, in AftFuselage. Refer to 30-10-00, Maintenance praclices,Paragraph 4.
€.f OU€
1\l'|,9.2J.
K.
M.
MECH INSP 2qr 4fi 800
Nlrt X
NIA X
Atlfr X
/D X
J>- X
N/n 1 .200 hours
/D X
/D X
,p X
il) X
1juX
;ib x
,U], X
ttX
EFFECTIVITY: ALL
5-20-05 .,"13?;333
//rt\i,!,r21 E,YJTttp / MAIN |ENAN C E
,s,,,A. ArcNAFTNA,5]INS ND I MANUAL
O. Pneumatic Deicer Boot Functional Check - \A/lng andEmpennage. Ref. 30-1 040, Maintenance practices,Paragraph 1.
Aft Fuselaoe (Station 452.00 to Station SS4.OO)
A. Flight Control System - Elevator and Rudder.
(1) Elevator and Rudder Torque Transfer Tubes.
(a) Attach points.
(b) Freeness of Bearings.
(c) Safety.
(d) Autopilot Servos - securig.
(e) Lubricate Control System. Refer to 12-2OeO,Maintenance Practices.
(2) PneumaticPlumbing.
(3) Structure.
B. Fuselage above Baggage Compartment.
(1) ElectricalBundles.
(2) Pneumatic Plumbing.
(3) Structure.
C. Electrical and Electronic Components.
(1) Long Range Navigation System.
(a) Security in Mountings.
(b) \Mre Bundles - damage and security.
(2) Electronic Engine Controls (Fuel Computers).
(a) Security in Mountings.
(b) Wre Bundles - damage and security.
(c) Inspect Air Filter ' cleanliness or obstructions.
MECH INSP M ,fdt 800
NIi' X
JY X
n/ X
)y X
_-v X
nht X
*v X
t/ X
-X-/- X
e) X
-tz X
^lA
x
itt, X
t/ X
s/ X
'gvX
EFFECTIVITY: ALL
5'20-05 ,"Ie?ffi33,[-
//rt\*[n21n,Y,t7tlp / MAINTENANaE
lsnAa.ArcnAFrNa.srm tm I MANUAL
EMPENNAGE - MAINTENANCE PRACTICES
1. Emoennaoe
A. Horizontal Trim Relays - security and electricalconnections.
B. Horizontal Stabilizer Trim Actuator.
(1) Attach Points.
(2) Electrical Connectrons.
(3) Ensure drain holes in bottom of actuatorare clear of grease and foreign matter.(lf water present, unit must be released.)
(4) Perform Horizontal Stabilizer Trim ActuatorInspection. Refer 2740-01, Inspection / Check.
C. Horizontal Stabilizer - condition and security.
(1) Attach Points - Forward and Afi.
(2) Upper and Lower Scissor Fitting Attach Points forlooseness.
(a) Shake Stabitizeiduring inspection.
(b) Inspect Scissors Assembly for cracks andsecurity.
(3) Check Stabilizer Aft Spar Sptice-Hinge FittingOutboard Lugs for cracks. Refer 5S-10-00,Maintenance Practices. Refer to FM AirworthinessDirective No. 89-12-08.
(4) Check Stabilizer Assembly for Radial and Axial play.Refigr to 55-10{0, Maintenance Prac{ices.
NOTE: This check is no longer required when thehinge improvements and scissors installationhave been accomplished per Service BulletinNo. 1124-55-021,Par|2. Para D thru F.
EFFECTIVITY: ALL
5-20-06 ,"I;?ff31
(5)
(6)
D.
//rt\mraa.wlit p / MAINTENANaE
ENAA ANCMF| I0Jg''fS LfO I MANUAL
Structure.
NOTE: Inspect structure for general condition,security, cracks, corrosion and loose ormissing rivets.
Lubricate Stabilizer. Refer 1 2-2G00, MaintenancePractices.
(a) Aft Hinge Fitting Bearings - 3 places preService Bulletin No. 1124-SS421 or 1 Dlace(intermediate bearing) on Aircraft 154,409,413,416,418,421,423,424 and 426 - 442withproduction modified hinge.
NOTE: Lubrication is no longer required whenhinge improvement has beenaccomplished per Service Bulletin No.I 1 24-55-02'1, Paragraph 2. D.
(b) Forward Scissors Assembly post ServiceBulletin No. 1124-55-021 (4 ptaces).
Elevator - general condition and security.
(1) Elevator Hinge Points.
(a) Check all Bearings for looseness, roughness,safety and general condition.
(b) Bonding Jumpers.
1 Condition, fraying and security.
2 Control Surface Bonding. Refer to23-6040, Inspection / Check.
(2) Elevator Torque Tube - security of attach points,universal joints and taper pins for looseness.
(3) Stop-Bolts and StopPads - condition and security.Check Travel Stops make contact in both direclionsof travel.
(4) Lubricate. Refer 12-20-O0, Maintenance Practices.
MECH INSP d 4A 800
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5'20-06 '.:31ir332
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EBAA ATRAFIng,.AiE,JD T MANUAL
F.
Refer to 27-20-00, lnspection / Check.
(5) Lubricate. Refer to 12-ZO-OO, Maintenance
G. Tail Skid - condition and security.
(5) Check for separation of skin to honeycomb.
Msually inspect upper and lower surface ofElevators for local bulging or looseness ofskins.
Tap test by lightly tapping skin with a coin orequivalent and comparing sound to adjacentlocations. Separation between skin andhoneycomb core can readily be identified byhollow sound to solidly bonded areas. Refer27-3O-OO,Inspection / Check, Paragraph 3.
Vertical Stabilizer - condition and security.
(1) Attach Points.
(2) Struc1ure.
Rudder - general condition and security.
(1) Rudder Trim Tab Actuators - attach ooints.
(2) Rudder Hinge Points:
(a) Check all Bearings for looseness, roughness,safety and general condition.
(b) Bonding Jumpers.
f Condition, fraying and security.
2 Control Surhce Bonding. Refer to23€0-00, Inspection / Check.
Rudder Attach Points - Stop-Bolts and Stop-pads -condition and security. Check Travel Stops makecontact in both directions of travel.
Rudder Trim Tab for excessive looseness and wear.
(a)
(b)
(3)
(4)
EFFECTIVIW: ALL
5-20-06 ,"13i;333
oon\ln Aa,wJittp / MATNTENANaE
anAE Arcatrrngusna uo I MANIIAL
Frame Station 540.00 and Ballast and Jack AdaDterMounting (if installed) - condition, damage and correctinstallation.
Tail Cone and Light - condition and security.
Static Discharge \A/icks and Bases - Vertical StabilizerCap, Rudder, Horizontal Stabilizer Tip and Elevator.
(1) Condition and security.
(2) Static Wck Inspection / Check.Refer to 23€0{0, Inspec{ion / Check.
(3) \Mck Base Bonding Inspection / Check.Refer to 23€0{0, Inspection / Check.
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EEAS,. ArcNAFT TI0.F rcOD I MANUAL
ENGINE. NACELLE AND PYLON . MAINTENANCE PRACTICES
N9IE All items in this section (5-2047) may be inspected at intervals of 300 hours to coincideith AlliedSignal Engine Inspections at the operators discretion.
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1. Enoine. Nacelle and Pvlon
A. Inspect inlet nacelle for cracks, loose dvets.corrosion, security and general condition.Refer 5440-00, Inspection / Check.
B. P2T2 Sensor.
(1) Condition and security.
(2) Heater Operational Test. Refer30-20-00, Maintenance Practices.
C. Inspect cowl structure, doors, skin andlatches for dents, cracks, fit, generalcondition and operation.
D. Inspect fire detector element for chafing,kinks, security and general condition.
E. Inspect low and high pressure bleed duct forleaks, cracks, fit and general condition.
NOTE: Inspect manifold assembly duringengine Major Periodic Inspection or\,vhenever the after body isremove0.
F" Inspect the following systems andcomponents for installation, clamping,security, condition, chafing, tube integrity,leakage and safety.
(1) Fuel Lines, Fuel Flow Transmitter,Pressure Switch.
EFFECTIVITY: ALL
5-20-07 ,"i3ffi33;
//rt\mrta,vTt p / MA1NTENANaE
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(2) Hydraulic Lines, Attenuator, HydraulicPump and Quick Disconnec{s.
(3) Hydraulic Pump - Remove DriveSpline, inspect and lubricate_ Refer29-10-00, Inspection / Check.
(4) Oil Pressure Lines. PressureTransmitter and Low pressure Switch.
(5) Electrical Wring, Connectors.
Inspect Engine Mount and Attachment forsecurity and general condition.
Visually inspect Jet Tail Pipe Nozzles fordents, cracks, bulges and general condition.
Check Engine Throttle System for freedomof movement, Control Cable routing,security of clamps, clearance and generalcondition.
Check Pylons and Firewalls for cracks,condition of Firewall Sealant, security ofHydraulic, Fuel, Electrical Connections andMechanical Feed-Throughs.
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5-20-07 ,"13?;333
//rt\.;t21F'YJlttp / MAINTENANaE
E'dlA, AftEAFf ,,g/gi'G LfD I MANUAL
THRUST REVERSER - MAINTENANCE PRACTICES
1. Thrust Reverser
NOTE: Deploy Thrust Reverser and installDeploy Ground Locks.
A. Wth Thrust Reverser Stang Covers andAccess Cover (Throttle Retarder FeedbackControl) removed, accomplish the following:
(1) Check Mechanical System includingThrottle Retarder Feedback Controland Actuator, Linkage for chafing,distortion, security and evidence ofwom bushings.
NOTE: Clean and lubricate ThrotfleRetarder Cable and Casing.Refer 78-32{0, MaintenancePractices.
(2) Inspecl Thrust Reverser generalcondition for cleanliness, FOD, fluidaccumulation, cracks and loose orworking fusteners.
(3) Inspect Thrust Reverser ActuatorMounting and Stop Bolts for securityand safety wire.
(4) Check Thrust Reverser Door Hingesand Bolts, Latch Hooks and Holes andFairings for dents, distortion, cracks,corrosion, loose or missing rivets,excessive wear, condition, securityand cleanliness.
(5) Lubricate Thrust Reverser Assembly.Refer 12-20-00, MaintenancePractices.
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5-20-08 ,"13|i331
//rt\mlln.w'lt p / MA1NTENANaE
dnAA, ArcAAFT /eIA'|''ireS LrD I MANUAL
(6) Check Thrust Reverser Outer CowlPanels for dents, distortion,cleanliness and loose or missingrivets.
(7) Check Thrust Reverser lnner DuctStructure for cracks, structuraldamage, loose or missing rivets,@rrosion, distortion and hot spots.
(8) Check Thrust Reverser HydraulicSystem, including Actuators andHydraulic Lines, Quick Disconnect forevidence of leaks, cracks, dents,clearance, chafi ng, tube integrity,condition and security.
(9) Inspect Thrust Reverser StangSupport Structure for structuraldamage, conosion and loose ormissing rivets.
(10) Check Thrust Reverser ElectricalSystem for cracked or burnedinsulation, loose connections andfrayed wires. Electrical components fordeterioration and broken or bent pins,security and cleanliness.
(1 1) Perform Operational Teston ThrustReverser System, including ThrustReverser Throttle Retarder FeedbackControl. Refer 78-30-00, MaintenancePractices, Paragraphs 2 and 3.
(12) 5000 Hour Thrust Reverser Inspection.Grumman (PMINSP-L84{1, availablefrom Gulfstream Aerospace).
(13) Perform Thrust Reverser SecondaryLatch Solenoid Switch Check. Refer78-30-00, Maintenance Practices.
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5-20-08 ,":Z1i,nZ
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ERAE ArcNAFTSIOI''iIB LN I MANUAL
AUXILIARY (LONG RANGE) FUEL - MAINTENANCE PRACTICES
1. Auxiliary (Long Ranoe) Fuel
A. Tank Area - general condition and leakage.
(1) Check Auxiliary Fuet System. Refer 28-5040,Adjustment / Test.
B. Structural Inspection - Disassemble the inboard side walland visually inspect the following:
(1) \A/all Attachment Points.
(2) \ /hll Two-Part Aftachment pins and Hinge.
(3) Inboard Side \A/all Supporting Structure.
(4) Attachment Points on Supporting Structure.
MECH INSP n 6 800
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ENAA, ATAAFf TIf,|I;'"E' ED I MANUAL
GENERAL - MAINTENANCE PRACTICES
1. General
A. Check that a Preflight Check has been made.
B. Check that all applicable FM Ainrvorthiness Directives arecomplied with.
C. Review manufacturers service data for applicability.
D. Check that all aircraft documents are cunent and in orderbefore release of aircraft.
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Customer: STARFLITE AVIATION A/C Type: WESTWIND
Part Name: RADOME Part No.: 5873000serial- No.: AUG-0017 P.O. No.: N83SG
G.O. No.: 1018383-OOO . Datr: rL/Ll/03Customer's Reason for Removaf i,lftKrro'-vlcustomer's Repair rnstructions RFRAT(
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THE NORDAM GROUP - TEXAS5l-01 BIue Mound RoadFt. Worth, TX 76t06
WORK ORDER
FAA Authorized Repair Station No. UE1R529K
) Approved
FINDINGS
(v) No
t_.)3.
Customer P.O. request: RePair.PN and SN verified. Identify as req.Damage:A) Repair 5rr outer surface defams atnose tip area IAW MNRP- 02 CHPT 1.B) Repair elongated holes as req.C) Repair damaged core with item 3A.Hardware:A) Replace missing/disbondingdiverters as needed Eo rePair.B) Return a new 3-M boot wiEh thisunit "uninstalled" . Customer instal-l-.C) Nc antenlaq 1pre-sc:nt, BAI'Paint: Apply prime and Paint as req.Other: Trans test radome IAW RTCA
DO-2]-3 ''SEE ATTACHEDII .
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5.6.
***
Customer,s Reason for Removal Confirmed, ( ) Yes ( ) No (X ) Not AppticableA.D. ts or Service Bul-fet,ins Incorporated ( ) Yes (\ ) No
Service Performed (.24) Repair ( ) Overhaul ( ) Other
THE AIRCRAFT COMPONENT IDENTIFIED ABOVE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH
CURRENT REGULATIONS OF THE FEDERAL AVIAT]ON AGENCY AldD IS APPROVED FOR RETURN TO
SERVICE WITH RESPECT TO THE SERVICE PERFORMED. PERTINENT DETAILS OF THE SERVICE
PERFORMED ARE ON FILE AT THIS REPAIR STATION T]NDER THE TEARDOWN REPORT NUMBER'
rNsPEcrroN APPRovA " fur"FORM Q0L2 REV. 2 tt-02-98
Customer:Cust. P.O.#Job#Teet Date:
/Yfu,Nttlltt-rIIts
Tranombeffi Test Report
STARFLITE AVIATIONN83SG101838$0001r30tc4
Test Freqrcncy 9.334 Ghz
Aircraft Type: WESII |INDPartNumber: 5873000SerialNumber: AU9-0017
RADOME CONDTT|oN
CONDITION
MAILIi{G ADDRESS
P.O. BOX 163E89
FORTWORTH. TX76f615101 BLUE IIIOUND ROAD
FT. WORTH, TX 76106
TELEPHOHE:(81 7)625-41 06
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FAA REPAIR STATION # UE1R529K
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TEL: 713 991'9lll' FA)C 713 991'9117
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Prlrtinent details ax€ on file atthis repai; sEiAuthorizBd InsPection Signature
Date of Final Inspection for Return to Sewice ? *j:e^aintenance Release Issu or NO
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FAA/UNITED STATESAUTHORIZED RELEASE CERTI FICATE
FAA FORI\4 8130.3, AIRWORTHINESS TAG
System Tracking Ref No :
39568
4. Consolidated Instrument &Avionics Co. pAl fns CnS * OSZnt 2ou JAA #4349510IndustrialAvenue Teterboro Airport Teterboro, New Jersey 0760g USA
POSITION TRANSMITTER c171813 Rere.ks Reterto Atlached Wolk Order fi ?q56g
Maintenance with Reference to:-
csl#149
dara and are in conditon lor s6le oDeEtion,Cerliares that unless olhe&ise sp€cified in 8locF13, the wi.k idenlrhed.n Btoc! l2 rnodescribed in block 13 was accomplished in accoroance wnh Tirte 14. Code o. Federalregulalions, part 43 and in respeci to thatwork, the ilems are approved for return lo
NSNr 0052-00-012.9005
.IIJESSM{
. Worthington Aviation Partso fnc.P.O. BOX 217172995 Lone Oak CircleSuite 10Eagan, MN 55121USA
8TJ39BAR-2 TRANSMITTER POSITION(EXCHANGE) Core Due:212812004
Core Charge: $0.00Core PN: 8TJ39BAR-2Core SN:
Credit Amounl $0.00
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SOLD TO: HOUSTON AVIATION8710 TRAVELAIRHOUSTON . TX 77061
PO #: 04-02-037
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PART #: 52-NBC2064YZP TORRINGTON
CERTIFICATE OF COMPLTA}TCE
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GENERAL CIYN.AMICSAviation Services'
REF. DOCUMENT:
PACKING LIST NUMBER:
Sales Order27484s2
Y5220 PAGE: 1DArE: 02 / 1-0 / 04
FRoM
Si.Hi't::t!:P:.
920-735- 70 0 0920-735- 7108
KC REP:CARRIER:
CARRIER ACCT:
FRT TERMS:FOB POINT:
WAYBILL:
SHIP DATE: FRT CHRG:
CERTIFICATION OF GONFORMANCEthe part ild/or componots idqtified on this shippq meat the cotrditiom ofthis sal6 ordq. Sellq funhq certiftes, or h6 o! filo its suppliq certification, that th6e wqe
md ae cosidsed to be in compliroce.to be shipped outside the UBited Stat6, S€llq or Sellq's mmufrctwq or suppliq certifiG that such parts ad compotr@ts comply with FoductioD requilem@ts
I acknowledge that I have r6eived the above parts md/br swicc i! good conditiotr.
RECEIVED BY
02/ao/04
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SET FORTH HEREIN AND ON THE
ffi'NGENEFIAL EIYNAMICSAviation Services'
REF. DOCUMENT:
PACKING LIST NUMBER:
Sales Order2748452
v5220
PHONE: 92FAX: 92
02/1-0/04 FRT CHRG:
PAGE: 2DArE: 02/LO/04
.00
FRoM
KC REP:CARRIER:
CARRIER ACCT:
FRT TERMS:FOB POINT:
WAYBILL:
SHIP DATE:
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I acktrowl€dge ftat I have rceived the above parts @d/or swic6 itr good conditioD
RECEIVED BY:
Sella haeby cotifia or hm ordetmined to be irWhoe the production
SET FORTH HEREIN AND ON THE REVERSE SIDEACCEPTED IN ACCORDANCE WITHSHIPPED BY:
9enbINSTRUMENTS*
'tOnOt Emery Avenue. Cleveland, OF| OO1rU
Ph: (216) 671-3133. Fax: (21Q) 671-4177
SQLD TO: General- DynanJ.cs Avlation Svcs*iF.$A Repair SrarJ.on.No. pJyR360Rii&8S. 34ttr ttrenue Sourh
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LIST.No.o7 \
lhDate ShippedfrAprtl 17, 2002
Customer P.O.# MSP-P0013145
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-CERTIFICATION.
ris is to certify that the part(s) furnished on this order arerw and have been manufactured In accordance with,plicable U.S. Military Specificatlons and FAA authorlzations.st and Inspection ieports are on file subject to examinatibn.
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Houston Aviation Technical Services t
BlloTraverair- .-'; vrvvo F'A'A'"
.< Houston, TX 770il
Repair station
# HOJRZ65K
- t jrr,. , artr,orer p.O. Customer Name U/.O.Lf?lq Ot*,,rr$Do siARtrLE,?at4o*-Xs+:ase or
. preliminary lnspection : - ,''w t --
Hidden Damgge Inspection :o CtzA -2k/re-
The aircraft component and /.or part.identified hereon has been inrpurtilaccordance with an approved specification "irirrolro, and is free ofdefects_in so far q; non _ destructivr€r';;>'"' 2.,-n k ;':Pr'T"FLo'du't revearr
This inspection does not incfud".o'irawings, state of wear, ,or tne prJiervation or tnis componentpfi\F
1 N001
Signed :
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SERVICEABLE PART
A€ PJ rzs-ETt3/O
WorkAccomolishd
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FG*"no*E nepaireo
D otner (Exptain)
THE AIRCRAFTAND / OR COMPONENT IOENTIFIED ABOVE WAS INSPECTED IN ACCOROANCE WITH CURRENTADMINISTRATION ANO IS APPROVED FOR BETURN TO SERVICE
PERTINENT DEIAILS ARE ON FIL'|(I THIS HEPAIR STATION,
UNDER WORK
KL-/o7{-
Signed D^t" c -2
UMTED BATTERIES AND ACCESSORTES, INC.CRS #U9BR6I8Y 7762 BRAI{IFF HOUSTON, TX 77061
TEL: 713 991-9lLl FAX: 713 991'9117E-IvIAIL : [email protected]
FORM #9007NiCad Battery Pack Work Order #
t , - -
.Curto^rr Date Receiv d \Zq -ojf Customer pg| P 833e1Battery Pack/CelVPower Supply fvffg. 5-& Mfg. Tlpe Ps v23'aT Mfg. Part No. SO | -io ?5'oI
Serial No. /3,tb' Pre-Service Hidden Damage Inspection
General Condition
In-Service Hidden Damage InspectionCapacity Tests, Step I J
End ef/. i 2nd
End of Disc
End of Discharge Voltage
Vol
End of Charge TFunctional TestReplaced
, Remarks f ' {J4JL l/14H+ +
.Work Accomplished B_ :-Ere - ' -ryfr?per CMM ( f- -
. Inspected By
lnspector RecommendationsThe aircraft component, appliance or accessory was in accordance with the current requirements of the
Federal Aviation Administration and is approvedlfufreturn to
Pertinent details are on file at this repair
Authorized Inspection SignatureDate of Final Inspection for Retum to Service Z-to ' I*o@orxo
SERVICEABLE PART(,
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MAINTENANCE RELEASE
THE AIRCRAFTAND / OR COMPONENT IDENTIFIED ABOVE WAS INSPECTED IN ACCOROANCE WITH CURRENTREGUTATIONS OF THE FEDERi{LA/|AT|ON AOMINISTRATION ANO lS APPROVED FOR RETURN TO SERVICEPERTINENT DEIAILST{RE ON flATTHIS REPAIR
UNDER WORK
Z-to -ofSign€d
UMTED BATTERTES AND ACCESSORTES, INC.cRS #U9BR618Y 7762 BRAIIIFF HOUSTON,TX7706I
TEL: 713 991-9Ltl FA)C 713 991-9117E-ldAIL : [email protected]
NiCad BatteryFORM#9007 I ^ -Pack TVork Order # b 3'] :
customer S:r:nr*-Li-\ e- Date ReceiveAP -o.{- Customer PO# l,J&gGBattery Pack/CelVPower Supply Mrg. lv\qMlr\lrrNJ Mfg. Type
Serial No. \J}A
Pre-Service Hidden Damage Inspection
General ConditionIteceivin g Voltage: Terminals
In-service Hidden I)amage Inspection
outer "*, prtulT"l.T,I;J,'ffu crses P,o. s Hot spots hLue<
Receptacle Assy. Qt,4 \ 5 Aup Fuse >L 10 Amp Fwe rP--
Mfg. Part No.'3 E*(- oc.l.}cr* <l\?.
Battery PacHl
Capdciry Tests, I throueh 3
I rstIlnd of Dischar Vol
Ilnd.of Discl Vol
i,lnd of Discharge VoltageF'INAL CHARGE
End of Charge Terminal Voltage 7 /: (@Irunctional Test PI{eplacedRemarks
WARRANTY: de if serviced a minimum of every 6 months'
Work Accornplished By per CMM
Inspected By
.:;
CompletionDate Z-/o -o flnspector Recommendationsj..heaircraflcomponent,uppl@in'pe't.ainaccordancewiththecunentrequirementsoftheFederal Aviation Administration and is approved for rettrm tgryrviPertinent details arc on file at this repair sta!,\uthorized Inspection Signaturel)ate of Final Inspection for Rettrm to Service rcsuaq6srxo
[osgrove flirclafl Seruice, Inc.
70 0$tff lttilltId[0[![gs, I[6il] ?3r-$ilr r
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TX 77A61
SHIP TO:STARFLITE MANAGEA{ENT GROUP9OOO RANDOLPHHOUSToN TX 77061
PACKING LIST33288
SHIP DAI€
)2-04-04DATE
02-04-04
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SERTAL NO.:ttAy82-270 F/T EXCH*
PTEASE USE oUR CX} * 026356{,HEAI RETURNING YOUR EXCHANGE CORE.
* RUNOUT CORES MUST BE RETURNED TA THE ]COSGROUE FACILI,TY INDICATED OAI THE ,CXO' -
TAG UITHIN 15 DAYS FROM THE DATE OFRECEIPT. ANY DELAY IN CORE RETURN MAYSUBJECT CUSTOA4ER TO A PENALTY CHARGE.IF A CORE REQUIRES PARTS A80UE A NOR/'4ALOVERHAUL, THE CUSTAMER WILL BE NOTIFIEDAND EILLED ACCORDINGT Y.
THANK YOU.
IF YOU FIND ANY PROBLEM UITH THIS SHIPMENTcAtt cusTol,fER sERuIcE AT ( 800 ) 645-l406.*****1**'r* THANK y0U FOR yOUR ORD6R *******
PLEASE NOTIFEES IMMEI'IELY IF ERROR IS
CHECKED BYTHIS COMPLETESYOUR ORDER
THIS IS A PARIIALSHIPMENT, SALANCETO FOLLOW
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I{O RETURNS ACCEPTED W|IHOUT PRIOR AUTHONIZATION, ALL iETURI{EO ATERIALS IAY EE AUAJECT TO A RESTOCKITIO FEE..'.-..-,_-a'?J
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FAA FORMS 813O-3AIRWORTHIN ESS APPROVAL TAG
USERN NSTALLER RESPONSIBILITIES
It is impodant to understand that the existence of this Document alone does not automatically con-stitute authority to install the parUbomponenVassembly.
Where the user/installer work in accordance with the national regulations of an AirworlhinessAuthority different than the Airworthiness Authority of the country specified in block 1 it is essentialthat the user/installer ensures that his/her Airworlhiness Authoriiy accepts parts/components/assem-blies frorn the Airworlhiness Authority of the country specified in btocf i. ' ' ' ,
Statements in block 14 and 19 dc not constitute irrstalfation ceffiication. ln all cases aircraft mainte-nance records must contain an installation certific3tion isgued in accordance with the nationa.l.regu-lations by'the user/installer before the aircraft may be flown.
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customer (ervFe T*Assembty t'tumoer rfl? o'4&Ocl-J,serial Nunoer'. ; h 4V(.8A - 27 O,Work Order No., /
Preliminary lnspection (List any damage found):
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Disassemble Brake 68@-&/,4.V'A@(GNJ. }A
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gi.,,Strip, Ciean & lrispect Piston Housing
I nspest Retating dises___
, I nspect Stationqry discs
illihspect Back & Pressure Ptates
InspectPistons@lnspect lnsulators & Screws
.ilnspect Grip & Tubes
ilnspect Return Spri#gs; Pins & Housings
Inspect Torque Tube
*i-'lnspect Hardware
tiMagnaflux Bolts
liltnsnect Plugs, Adapters & Bleeders
rRe-Pad back & Pressure Plates @Re-Paint Piston Housing,:.i
flppfy Sandstrom To Bolt Shanlis
ble Brake:r!,... /brque Brake Bolt Nuts..ir',i';q,
Pressure Checked At
nning Clearance oo f]inhTcian Sign:
tenariLe Release Signed By lnspector:
Final Inspection
J ooo PSI . .qe(o PSI (Back Pressure)
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Tif UN;yERSAI:AVIOIV/CS rer:(szo) 2ss'2300 (800)32r's253Y yy liiil'S--C O n p O [nr tb 1 ArizonaDivision Fax:(520)295-2395
WORKORDER
04R08875Repair Station UZNR483N
Claim DateClaim NoDiv-P1ant
02/11 /20040440887502-20
PageAck. No
1
0 40231 0
Received FromShip ToPart NoPart DescrReason
DO260O DUNCAN
DO26O2 DUNCAN
AVIONICS--HOUSTONAVIONICS--HOUSTON
PhonePhone
1013-42-011IM, BLK, ANA, RAIM, 429 GPS OUT
CM REPAIR/MODIFY, NON-WARRANTY
Part SerialI{arranty NoExpires
548
C Serial F].eetTypeRegistration
A/c DescrWCRK ORDER SUMMARY
CUST REPORTED: BATTERY DISCREPANCYREPAIR ACTION: BOARD REMOVED/REPAIRED AND
DURING TEST ENCOUNTERED: BATTERY DISCREPANCYREPAIR ACTION: BOARD REMOVED/REPAIRED AND
REPATR ACT]ON: BOARD REMOVED,/REPATRED AND
REINSTAI,LED
REINSTALLEDREINSTALLED
OUTGOING CONFIGURATIONPART NO:SERIAL NO:c aNl
brJMODS.DisplayMONITORAUXARINC
1013-42-01154823 .010. 3
2,3, 4,51.11.31.33.0
WORK ORDER DETAIL
>CUST REPORTED BATTERY DISCREPANCY< BATTERY FAIL MESSAGE.
OUTGOING: SCN 23.0REPAIR/MODIFY, NON-WARRANTY
SHIP DATE: 02/18/2004DO NOT SHIP-SEE BELOW
EXPEDITE
EMPLOYEE NAME
WORK PERFORMED
DATE HOURS
INCOMINGSCN
GPSMODS.MONlTOF.AUXARINCNOTE:
OO1 GARLANT. INC INSPUNIT ALLPAINT ON
COLORED)SLIGHTLY
OO2 FINNEY
CONFIGURATION23 .010.2zrJ'11.3I.23.0W,/FLASHCARD
JR BERNARDO
AT 1503 LAST INSP DATE: 03,/26/1991 SCRATCHED
OVER. VERY DIRTY LENS WITH ELASH LIGHTLY CHIPPED
FACEPLATE. EDGES. FRONT. MISSING HARDWARE (Al'lBER
ABOVE "MSG' KEY.LOOSE LENS
DENNIS VJ
CONTINUED ON NEXT PAGE
02/L1 /2004 0.10
02/]-8/2004 0. 10
i(V 5YSTE MS COR PORAT ION ArizonaDivision
3260 East Universal Way, Tucson, Arizona 85706 U.S.A.Tel: (520) 29s-2300 (800) 321-s253
Fax: (520) 295-2395
WORKORDER
04R08875Repair Station UZNR483N
Clai-rn DateClaim NoDiv-Plant
02 /r'7 /20040440887502-20
PageAck. No
t
04023't 0
Received FromTo
Part NoPart DescrReasonA,/C Serial
DO26OO DUNCAN
DO26O2 DUNCAN
AVIONICS--HOUSTONAVIONICS--HOUSTON
PhonePhone
: 1013-42-0111M,BLK,ANA,RAIM, 429 GPS OUT
CM REPAIR/MODIFY, NON-WARRANTY
Part SerialWa*anty No
FleetryP€Registration :
A/C Descr i
SQUAWK VERIFIEDREPLACED BATTERIES TO CORRECT.
INSTALLED AUX 1.3, GPS 10.3.REMOVED PART: CPU BOARD
0l-013010A s/N: 93170-08 w/o + 04R08875-001REPLACE BATTERY (P/N ?8036005) DUE TO LOW VOLTS
REMOVED PART: DISPLAY BOARD01013060A s/N: 92731-40 w/o * 04R08875-002
BOARD REMOVED FOR LATEST ECO UPDATES
REMOVED PART: GPS BOARD
010130?5c s/N: 92707-03 w/o # 04R08875-003REPLACE BATTEF.Y (P/N 78036005) DUE TO LOW VOLTS
BOARD REMOVED FOR LATEST ECO UPDATES
OO3 FINNEY DENNIS W
REPLACED MISSING AMBER LENS IN MSG LfGHT.TNSTALLED to*t;r.3l3o?3fl3r*, e31?0-08 w/o * 04Ro8B7s-001
work performed on board:>PERFORMED THE FOLLOWING:REPLACED COMPONENT: BT1
- PART NUMBER: ?8036005- REASON: OUT OF TOLERANCE<
Inspected: No Def.ects
INSTALLED PART: DISPLAY BOARD
010130604 S,/N: 92'7 3I-40Work Performed on board:
>PERFORMED THE FOLLOWING:COMPLETED ECO(S) : 101295<Insoected: No Defects
l
INSTALLED PART: GPS BOARD
w/o # 04R08875-002
O1O13O?5c S/N: 9270?-03 w/o # 04R08875-003Work Performed on board:
>PERFORMED THE FOLLOV{INGrREPLACED COMPONENT: BT1
- PART NUMBER: 78036005- REASON: OUT OF TOLERANCE<
>PERFORMED THE FOLLOWING:COMPLETED ECo(S) : 102340<InsPected: No Defects
VERIFIED UNIT CIRCUIT BOARD CONFIGURATION
OVERHAULED AND REPAIRED IN ACCORDANCE WITH UNIVERSAL
AVIONICS MAINTENANCE MANUAL 34-60-I'1. TESTED TO CURRENT
MANUFACTURING ACCEPTANCE TEST PROCEDURES (ATP), REPORT
20062. PASSED ATP.DATABASE DATE: 03/17l04 REGION: world
CONTINUED ON NEXT PAGE
02 /18 /2004 2.OO
I
)fl( 3260 East Universal Way, Tucson, Arizona85706 U.S.A.
T|fiUNTVERSACA/IO,A/ICS ret:(szo) zss'2300 (800)32r-5253V i'!i-e il"S-b o n p O tiAT lb N ArizonaDivision Fax:(520)295-2395
WORKORDER
04R08875Repair Station UZNR483N
Claim DateClaim NoDiv-PIant
02/L1 /20040440887502-20
PageAck. No
3
040231 0
Received FronTo
Part NoPart DescrReason
DO26OO DUNCAN
DO26O2 DUNCAN
AVIONICS-_HOUSTONAVIONICS--HOUSTON
PhonePhone
1013-42-0111M, BLK, ANA, RATM, 429 GPS OUT
CM REPAIR/MODIFY, NON-WARRANTY
Part SerialWarranty NoExpires
C Serial F1€etryPeRegistration
A/C Descr02/19/2004
02/79/2004
0. 10OO4 PROCTOR BARRY
POST-MAINTENANCE INSPECTION PERFORMED.
APPLTANCE PASSED INSP IAW INSPECTION PROCEDURES REPORT # 20430.INSPECTION COMPLETED AT 0925.
OO5 FROEHLICH III WILLIAM JFINAL INSPECTION PERFORMED.
APPLIANCE PASSED INSP TAW INSPECTION PROCEDURES REPORT * 20430.INSPECTION COMPLETED AT 0925.THIS ARTICLE IS AIRWORTHY W]TH RESPECT TO THE WORK
PERFORMED.
0. 10
Tech
RpmnSupv
Maint
RpmnPerfFinafInsp
FINNEY DENNIS W
LLIAM J
FROEHLICH III WILLIAM J
2552'109Date: A2/19/2004
Date: 02/19/2004
Date: 02/19/2004
Date 02/19/2004
255]-26r
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EnAa. AncnAFrnnsrrctm I IWANUAL
1.
NOTE: All items in this section (5-21-00) are to be inspected at 1S0 hour intervals.
Enoine
Engine Periodic Inspection. Ref. 72-00-00, Inspection/Checksection of applicable Alliedsignal Aerospace Light MaintenanceManual.
NOTE: For Engine, Nacelle and Pylon Inspection, Ref. 5-20-07,Maintenance Practices.
Starter/Generator
A. Electrical Leads and Cooling Duct - condition and security.
B. Cooling Fan - nicks and blade damage.
C. Brushes Wear Check - Ref. 80-10-00, MaintenancePractices and/or Lucas Aerospace Maintenance Manual,File No. 23700.
3. General
A. Check that a Preflight Inspection has been made.
B. Check all applicable FAA Ainrorthiness Directivesand Manufacturers'Service Bulletins. Make required logbook entries.
C. Check that allaircraft documents are cunent and in orderbefore release of aircraft.
LEFT RIGHT
[/|ECH INSP MECH INSP
*/ tu .v 4.x* ry J2* h'Y
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H utr "Xnlr
W /2( Iq 4
01
//7
EFFECTIVITY: ALL
5-21'00 ""il1irti,
Shoreline dba Safetech?Houston Branch - FAA WV1R599K8305 Monroe Road
, Houston, TX77061" 713-947-1115 713-947-0593 (fax)
Work Order No: AH274'l'l
r Rec'd: 1111012003 Date Shipped: I I Date Reqd: 111'1712003
Customer: STARFLITE MANAGEMENTGROUP
Account Gode: CREDIT CARD-COD
Gust# 89S
Gustomer P.O. # 83SG
Instructions: RECERTIFy
Part Description: LIFEVEST, ADULT/CHILD
SerialNo: VARIOUS
Qty: 9 MFR.#:
AdditionalSerial No:
MFR: VARIOUS
VARIOUS
Teardown Finding: NORMAL WEAR,
Gorrective Action: AIR RETENTION TESTED, WEIGHT CHECKED C02 CART., CHECKED LIGHT ASSY., REPACKED PER MFG CMM
25-60-6 25-60-7
Date Completed: 11 117 12003 Tech: LM Inspector: M
THE COMPONENT IDENTIFIED ABOVE IS APPROVED AIRWORTHY WITH RESPECT TO THE WORK
Paoe 1 of 1 CUSTOMER COPY
Shoreline dba SafetechHouston Branch - FAA WV1R599K
8305 Monroe RoadHouston, TX77061
7 13-947 -1 1 15 7 13-947-0593 (fax)
PACKING LISTSOLD TO: STARFLITE MANAGEMENT GRoUP
9OOO RANDOLPHHOUSTON TX77061USA
SHIP TO: STARFLITE MANAGEMENT GROUPHOLDMILL CALL
Date
11t17t2003
Purchase Order No
83SG
Requisition No Work Order No
4H27411
Salesperson
REECE
Account No
895Terms
CREDIT CARD.COD
FOB
HoustonDate Shipped Shipped Via
WILL CALL
Tracking No
Product
LIFEVEST, ADULT/CHILDMFR
VARIOUSMFR #
VARIOUSSerial Number
VARIOUSPart Number Description ary Prlce Amount
lsER-AssoRITOTAL
LIFEVEST SERVICE, ASSORTED MFG. 9.37 84.33
84.33
SHORELINE MARINE, INC. dla SAFETECH9305 Monroe
Houston, Texas 770617t3-947-ins
FAA Repair Station WVIRSggK ouo- vCustonref LIFE VEST LOG
Pa4 Nlmber
::5{r:)q
t
t
ciq)
MAINTENAN
for rerum to service.
FORM SS30r 09/29/01
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