BRITISH MICROLIGHT AIRCRAFT ASSOCIATION MICROLIGHT TYPE ACCEPTANCE DATA SHEET NO: BMO-33 ISSUE: 1 RAVEN/PUMA

Transcription

1 BRITISH MICROLIGHT AIRCRAFT ASSOCIATION MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) TYPE: RAVEN/PUMA (1) MANU F ACTU RER: Wing: Southdown InternationalLtd (UK) Trike: Ultrasports Ltd (UK) (2) UK IMPORTER: N/A (3) CERTIFIC_ATION BASIS: BCAR Section S requirements listed in CAA document dated 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 (ine canard 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: m m 1.37 m 148 kg 343 kg 9.83 kg/m kg/m2 20 litres DOCJJMENLIS$UE STATUS Issue RevIsion Date Authorisation Pages Valid pages at this l\umber Reference affected Issue number 1 1 New B It All new Page No. Page Issue laan 1149.!o /. J ' TAOS BMD-33 Page 1 of 8.

2 (6) POWERPU\NTS MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) Designation Raven/ Puma Engine Type Fuji Robin EC44PM. Invtd Reduction 2.8:1 Gear/ratio Exhaust System Nicklow Intake - System Propeller Type Laminated wood Propeller 62" x 36" Dia x phea Noise Type 32M Cert. No. Issue 1. Designation " Englne Type Reduction Gear/ratio Exhaust System Intake System Propeller Type.. Propeller Dia x Pitch Noise Cert. Type No. Noise reauirement: Reqistered Pre 1/4/86 80 dba Reqistered Post 1/4/86 76 dba 8JL9JI8 BeAR Reference N Iss 4 N I ss-'l, TAOS BMQ-33 Page 2 of 8.

3 MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) (7) MANDATORY LIMITATIONS: (* indicates which are placarded) *(a) Max Take-off Weight: 343 kg *(b) (c) C G Limits: C G Datum: Nj A - weightshift *(d) Cockpit Loadings Front Rear Total Pilotor Ballast (min) 75 kg Pilot or Ballast (max) 90 kg - kg 75 kg 90 kg 180 kg (e) (f) *(g) ( *(h) *(i) *(j) ( k) Permanent Ballast, Weight and Position: Not fitted. Empty C G: Never Exceed Speed: 90 mph, Manoeuvring Speed: 60 mph Manoeuvre Limitations: Aerobatics prohibited. Roll <600 ban k Pitch <+j- 30 Fuel Contents (Max Usable): 20 litres Power Plant: See Table below ENGINE Fuji Robin EC44PM Max RPM 6800 Max CHT N/A Max EGT N/A Fuel Spec 92 Oct (min) Petrol/oil Engine Self mix Oil Soec 2 stroke Gearbox N/A Oil Soec Fuel/Oil Mix 40:1 ' Oil Pressure N/A I Oil Temp N/A Coolant Temp N/A TAOS BMD-33 Page 3 of 8.

4 MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) (8) INSTRUMENTS REQUIRED FOR TYEACCEPTANCE: ASI Altimeter RPM CHT Req ui red Req ui red Req ui red NjA 0 to >90 mph Wrist type or equivalent acceptable Compass EGT CoolanLJemQ NjA NjA NjA (9) CONTROLDEFLECTIONS (3-AXIS SYSTEMS): NjA - weightshift Pitch Control TailDlane Trim Ailerons Rudder SteerinQ oilis 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.

5 . MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TAOS) Note: Drawings and/or colour photographs illustrating the principal features of the aircraft described herein, shall be attached to, and form part of, this Data Sheet. Issue Authorisation Date BMAA /) g mill! / f) J),J. C-(2;?'1?r / f J p r "\; " BLANKIS4.TAD TADS BMQ-33 Page 5 of 8.

6 MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TAOS) T ADS No BMO-33 Issue 1 APPENDIX 1 APPENDIX 1 As a result of the BMAA review, certain features of the Raven/Puma are required to have been modified and others also require the particular attention of responsible inspectors. These features are listed below and further information is given in BMAA Documents TS.001 at Issue 3 or later and/or TIL 0007; where appropriate the relevant document is nominated 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 on wing 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 Fire resistant fuel lines near engine, as Document TIL Series No An on-off fuel cock, as Document TS.001. (" Fire resistant ignition switch wiring, as Document TIL No Whilst the type satisfies the intent of BCAR Section S, a placard must be installed as follows:- OCCUPANT WARNING:- THIS AEROPLANE HAS NOT BEEN SHOWN TO COMPLY WITH ANY PUBLISHED CODE OF AIRWORTHINESS. Inspection Inspectors must also pay particular attention to the following:- S 605 (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. S 607 Propeller shaft lock nut, as Document TS.001. S 627 Check for cracking at the seat frame attachment, as Document TS.001. S 775 Check windshield, if fitted, as Document TS.001. S 785 Check safety harness/seat belt and attachment, as Document TS.001 and also see TIL Series No 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 and S 975 Fuel tan k installation, as Document TS.001. S1301 EQuipment function The suitability, function and safe installation of equipment installed must be checked by inspection for each aircraft. In addition, inspectors attention must be paid to those items listed in the BMAA Inspector's Manual and those Bulletins or Defect Warnings highlighting individual components used on the machine. Such items as have been issued (at first issue of this document) which are particularly relevant to versions of similar tri kes to that of the Raven/Puma are also highlighted in BMAA Document TS.001. TAOS BMQ-33 Page 6 of 8

7 ,;\.-5mm "0/0 x 8 S,W,G, SlEELINNERlUBE Not t 0,8 C ale HAINlUBE 2 II" % x 17 S,W,G, aj 3: 2,63:\ RA1IO AS fltuii STANnARD 11"IN ENG H1G BRMKETS 3/'," x 15 S,W,G, SaEL BOx. 1000mm 2 1/8"0/0 x 11 S,W,(j, I DOUBLESLEEVEDI," 1 3/1, (JIll x y-all BRA(ltlG WIRES 8 S W,I;, ttljl11 SfRAUD san, DOUBLESWAGE(J 3:... n ::0 0 r z... 0 (;1.. :J: aj 3: 0 -< I " VJ ft1 VJ n... n (J) ft1 (J) " c: CD Z f-' n ft1 0 " OJ \D co "",lnilnl_!ir.i"a,,,--, l, 1- "", - \670mm llialk '/::':fs -I '1J '1J CD :J Cl- 1-" X N lf1 :r: ft1 ft1 0 lf1 -..J 0 "'" CD TYPICAL PUMA TRIKE For guidance with regard to primary structure - other details vary..

8 B M A A MICROliGHT TYPE ACCEPTANCE DATA SHEET (TAOS) NO: aho-33 Issue 1 ppendix 2 continued 1 I I (Jo k, \31;:-,;? t1j G \ 0- ",J " X I( o. IU ru ::- 01 \4 <'G - (:IIGIJ.;;:;/ i \. \ 't 0 ". OJ 11,. IN i r '. 8 (\J',..r III '". 1'-.8 (, - T -.,-..- \.. r-.. 'I', (\I. -,J I." ". -'=-:.= "I r' ".J!'-3 ("1-- "", ".:-.: I I I -:;0:-.L--&,.., "", i -,L6- '-j -, Not to scale RAVEN WING Page 8 of 8