MICROLIGHT TYPE ACCEPTANCE DATA SHEET · On the Raven wing: Flying wire diameters increased to 4mm; Additional sleeving on wing leading edge; Extra batten on lower surface of wing..

BRITISH MICROLIGHT AIRCRAFT ASSOCIATION

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-33 ISSUE: 1

TYPE: RAVEN/PUMA

(1) MANU F ACTU RER: Wing: Southdown InternationalLtd (UK)Trike: Ultrasports Ltd (UK)

(2)

(3)

UK IMPORTER: N/A

CERTIFIC_ATION BASIS: BCAR Section S requirements listed in CAA documentdated 17th January 1986, ref: 9/30/UL 18

(4) DEFINITION QF BAS_IC DESIGN STANDARD: Not available (but see appendix)

(5) DIMENS_IOJ"I/~ElfiHTS_FQR COMPLIANCE WITH MICROLIGHT DEFINITION

(a) Win g area (inecanard area, excludingwinglets):(b) Span:(cr) Standard Mean Chord:(d) DrY' Empty Weight:(e) Max Take-Off Weight:(f) Wing Loading (Weight Empty/WingArea):(g) Wing Loading (MaxTake-Off Weight/WingArea):(h) Fuel Capacity:

15.05 m210.97 m1.37 m148 kg343 kg9.83 kg/m222.79 kg/m220 litres

DOCJJMENLIS$UE STATUS

TAOS BMD-33 Page 1 of 8.

Issue RevIsion Date Authorisation Pages Valid pages at thisl\umber Reference affected Issue number 1

1 New 10.12.93 B It All new Page No. Page IssuelAAN 1149 .!o

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1 12 13 14

' 15 16 17 18 1

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-33 ISSUE: 1

(6) POWERPU\NTS

Designation Raven/Puma 1 2 3 4 5

Engine Type Fuji RobinEC44PM. Invtd

Reduction 2.8:1Gear/ratio

Exhaust NicklowSystem

Intake -System

Propeller LaminatedType wood

Propeller 62" x 36"Dia x pheA

Noise Type 32MCert. No. Issue 1 .

Noise reauirement:

~Reqistered Pre 1/4/86 80 dBA

Reqistered Post 1/4/86 76 dBA

~~8JL9JI8

BeAR Reference

N3-6. 3 Iss 4

N3-6. 4 I ss-'l,

TAOS BMQ-33 Page 2 of 8.

Designation6 7 8 9 10

"

Englne Type

ReductionGear/ratio

Exhaust

System

Intake

System

PropellerType

..

PropellerDia x Pitch

Noise TypeCert. No.

(7)

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-33 ISSUE: 1

*(a)

MANDATORY LIMITATIONS: (* indicates which are placarded)

Max Take-off Weight: 343 kg

*(b)

(c)

*(d)

(e)

(f)

*(g)(

*(h)

*(i)

*(j)

( k)

C G Limits: Nj A - weightshift

C G Datum:

Cockpit Loadings Front

Pilotor Ballast (min) 75 kg

Pilot or Ballast (max) 90 kg

Permanent Ballast, Weight and Position: Not fitted.

Empty C G:

Never Exceed Speed: 90 mph

, Manoeuvring Speed: 60 mph

Manoeuvre Limitations: Aerobatics prohibited. Roll

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-33 ISSUE: 1

(8) INSTRUMENTS REQUIRED FOR TY~EACCEPTANCE:

Compass EGT CoolanLJemQ

NjA NjA NjA

(9) CONTROLDEFLECTIONS (3-AXIS SYSTEMS): NjA - weightshift

Pitch ControlTailDlane TrimAileronsRudderSteerinQ~oil~IS

Up:Up:Up:Left:Left:NjA

Down:Down:Down:Right:Right:

(10) PILOT'S NOTES. MAINTENANCEMANUALS REFEREN_CES:

BMPyAdocuments: MAAN1149 and TS.OO1

(11) MANDATORYMODIFICATIONS/SERVICE BULLETINS/AIRWORTHINESS DIRECTIVES. ETC: .See Appendix 1

(12) APPROVED OPTIONAL MODIFICATIONS

(13) MINIMUM PERFORMANCE AT MAX T /0 WEIGHT:

Rate of Climb: ~ 400 ftj min ute

Climb speed: 45 mph

Stall or Minimum Flying Speed: 38 mph

TAOS BMO-33 Page 4 of 8.

ASI Altimeter RPM CHT

Req ui red Req ui red Req ui red NjA0 to >90 mph Wrist type

or equivalent acceptable

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TAOS)

NO: BMO-33 ISSUE: 1

Note: Drawings and/or colour photographs illustrating the principal features ofthe aircraft described herein, shall be attached to, and form part of, this DataSheet.

IssueAuthorisation

Date BMAA

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BLANKIS4.TAD

TADS BMQ-33 Page 5 of 8.

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TAOS) TADS No BMO-33Issue 1

APPENDIX 1APPENDIX 1

As a result of the BMAA review, certain features of the Raven/Puma are required to havebeen modified and others also require the particular attention of responsible inspectors.These features are listed below and further information is given in BMAA DocumentsTS.001 at Issue 3 or later and/or TIL 0007; where appropriate the relevant document isnominated below for each matter.

Modifications The following are to have been incorporated:-

S 603

S 627

S 786

S 901

S 967

S 993

S 995

S1141

S 1541

Tri ke monopole (pylon) back-up cable, as Document TS.001.

On the trike structure, minimum standard, as Document TS.001.On the Raven wing: Flying wire diameters increased to 4mm; Additional sleeving onwing leading edge; Extra batten on lower surface of wing. .Note: Raven wing specification as per Medway Microlights.

Protective coati ng of welded steel components, as Document TS.001.

Safety helmet placard, requiring helmet to be worn when flying the aeroplane.

Attention to reduction drive, as appropriate, as Document TS.001.

Fuel tank drip tray installation, as Document TIL Series No 0007.

Fire resistant fuel lines near engine, as Document TIL Series No. 0007.

An on-off fuel cock, as Document TS.001.("

Fire resistant ignition switch wiring, as Document TIL No. 0007.

Whilst the type satisfies the intent of BCAR Section S, a placard must beinstalled as follows:-OCCUPANT WARNING:- THIS AEROPLANE HAS NOT BEEN SHOWN TO COMPLY WITH ANY PUBLISHED CODE OF AIRWORTHINESS .

S 605

Inspection Inspectors must also pay particular attention to the following:-

(i) The satisfactory condition of welds, as Document TS.001.(ii) :;Axle tie wires and their security, as Document TS.001.(iii) Tri ke keel at rear footrest attach position, as Document TS.001.

Propeller shaft lock nut, as Document TS.001.

Check for cracking at the seat frame attachment, as Document TS.001.

Check windshield, if fitted, as Document TS.001.

Check safety harness/seat belt and attachment, as Document TS.001 and also seeTIL Series No 0006.

S 901 Power unit installation features, as Document TS.001.

S 925 Propeller clearance, as Document TS.001.

S 951 Fuel line layout, as Document TS.001.

S 959, S 967 andS 975 Fuel tan k installation, as Document TS.001.

S1301 EQuipment function The suitability, function and safe installation of equipmentinstalled must be checked by inspection for each aircraft.

In addition, inspectors attention must be paid to those items listed in the BMAAInspector's Manual and those Bulletins or Defect Warnings highlighting individualcomponents used on the machine. Such items as have been issued (at first issue of thisdocument) which are particularly relevant to versions of similar tri kes to that of theRaven/Puma are also highlighted in BMAA Document TS.001.

S 607

S 627

S 775

S 785

TAOS BMQ-33 Page 6 of 8

Not t 0 ,8 C ale

1 2 118"0/0 x 8 S,W,G,

,;\.-5mm SlEELINNERlUBE

HAINlUBE2 II~" % x 17 S,W,G,

2,63:\ RA1IO AS fltUII STANnARD,"

11"IN ENG H1G BRMKETS3/'," x 15 S,W,G,SaEL BOx.

1000mm2 1/8"0/0 x 11 S,W,(j,I DOUBLESLEEVEDI

1 3/1, (JIll xy-All BRA(ltlG WIRES

8 S W,I;, ttlJL11 SfRAUDsan, DOUBLESWAGE(J

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-..J TYPICAL PUMA TRIKEFor guidance with regard to primary structure - other details vary.

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B M A A MICROliGHT TYPE ACCEPTANCE DATA SHEET (TAOS)

NO: aHO-33

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