BRITISH MICROLIGHT AIRCRAFT ASSOCIATION MICROLIGHT TYPE ACCEPTANCE DATA SHEET NO: BMO-28 ISSUE: 1. (G-MJCU - only example of type)

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1 BRITISH MICROLIGHT AIRCRAFT ASSOCIATION MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) TYPE: TYPHOONJTARJANI TRIKE (G-MJCU - only example of type) (1 ) MANUFACTURER: Wing: Solar Wings Ltd (UK) Trike: F. Tarjani (UK) (2) UK IMPORTER: NjA (3) CERTIFICATION BASIS: BCAR Section S requirements listed in CAA document dated 17th January 1986, ref: 9j30jUL18 (4) DEFINITION OF BASIC_DESIGN STANDARD: Not available (but see appendix) (5) DIMENSIONS/WEIGHTS FOR COMPLIANCE WITH MICROLIGHT DEFINITION (a) Wing area (inccanard area, excludingwinglets): (b) Span: (c) Standard Mean Chord: {". (0) m..y Empty Weight: (e) Max Take-Off Weight: (f) Wing Loading (Weight Empty/WingArea): (g) Wi n g Loadi n g (MaxTake-Off Weight/WingArea): (h) Fuel Capacity: m m 1.54 m 85 kg 205 kg 5.52 kgjm kgjm2 15 litres. DOCUMENT.ISSUE STATUS Issue RevisIOn Date Authorisation Pages Valid pages at this Number Reference affected Issue number 1 1 New HAAN1135 B. \ I - ", } '"... tjlfj All new Page No. Page Issue TAOS BMo-28 Page 1 of 8.

2 (6) PQWERPLANTS Designation Typhoon/ Tar] ani Tri ke Engine Type Fuji Robin EC25PS. Invtd Reduction 2.32:1 Gear/ratio MICROLIGHTTYPE ACCEPTANCE DATA SHEET (TADS) Exhaust Nicklow ' System Intake - System Propeller Type, Laminated wood Propeller 52" x 28" Dia x Pitch Noise Type 108M Cert. No. Issue 1. Designation " Engine Type Reduction Gear/ratio Exhaust System Intake, System \ Propeller Type Propeller Di a x Pitch Noise Cert. Type No. ~Qi5e requirement: - 1 Seat ReGistered Pre 1/4/86 80 dba ~egistered Post 1/4/86 76 dba 2 Seat ~ llildba BCAR Reference N Iss 4 1Ij:l~6. 4 I s s 4- TAOS 8M0-28 Page 2 of 8.

3 MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) (7) MANDATORYLIMITATIONS~ (* indicates which are placarded) *(a) Max Take-off Weight: 205 kg *(b) (c) C G Limits: C G Datum: N/A - weightshift *(d) Cockpit Loadings Front Rear Total Pilot or Ballast Pilot or Ballast (min) (max) 55 kg - kg 55 kg 90 kg - kg 90 kg (e) (f) *(g) Permanent Ballast, Weight and Position: Not fitted. Empty C G: Never Exceed Speed: 55 mph *~~h) y Manoeuvring Speed: 55 mph *(i) *(j) (k), Manoeuvre Limitatio~s: Aerobatics prohibited. Roll <600 ban k Pitch <+/- 30 Fuel Contents (Max Usable): 15 litres. Power Plant: See Table below ENGINE Fuj i Robi n EC25PS Max RPM 6500 Max CHT Max EGT N/A N/A Fuel Spec 92 Oct (mln) Petrol/oil Engine Self mi x Oil Soec 2 stroke Gearbox N/A Oil Soec Fuel/Oil Mix 40:1 \ Oil Pressure N/A Oil Temp N/A Coolant Temp N/A TADS BMo-28 Page 3 of 8.

4 MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) (8) INSTRUMENTS REQUIRED FOR TYPE ACCEPTANCE: ASI Altimeter RPM CHT Required Req ui red Req ui red NjA 0 to >55 mph Wrist type or equivalent acceptable Compass EGT Coolant TemQ NjA NjA NjA (9) CONTROL DEFLECTIONS (3-AXIS SYSTEMS): NjA - weightshift Pitch Control Tailplane Trim Ailerons Rudder Steerino Spoilers Up: Up: Up: Left: Left: NjA Down: Down: Down: Right: Right: '(10) PILOT'S NOTES. MAINTENANCEMANUALS REFERENCES: (, y BMAAdocuments: MAAN1135, WS.003 and TS.006 (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: ~ 300 ftj min u te Stall or Minimum Flying Speed: 28 mph TAOS BMD-28 Page 4 of 8.

5 MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) 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 Autho:r:isation Date BMAA / 3!tIR/l I'f-,2J~~~4r 9r~ f- " "., BLANKIS4.TAD TAOS BMO-28 Page 5 of 8.

6 MICROLIGHT TYPE ACCEPTANCEDATA SHEET (TADS) APPENDIX 1. ADDITIONAL DOCUMENTATION The Typhoon/Tarjani Tri ke must satisfy the modification and inspection provisions set out in BMAAdocuments WS.O03 and TS.006 (latest issue). The areas affected are as. follows: a) Modifications: S 605 E i) Wing attachment bracket. ii) Front strut. S 627 Non flexible coating. S 786 Safety helmet placard. S 901 Power plant installation, carburettor support. S 993 d) Fuel li nes. S 995 Fuel cock. S 1141 E Ignition switch wiring. S ) Airspeed indicator.. S )Altimeter placard (where applicable). S 1541 pthe,r placards. b) InsQection: S 603 S 605 S 607 S 609 S 623 S 626 S 627 Basic structu re of tri ke.. E Welds on engine supports, seat frame, and front wheel assembly. Wing batten retainers. Self locking propeller shaft nut (if fitted). (Wing): Keel. Sail fabric. Negative load bracing wires. Hang channels and trike attachments. Cables swages and rigging cables. Oversleeving of control frame uprights and cross bar. Nose catch to be inspected. S 785 Safety harness/seat belt and attachments. S 901 b) 1) Power plant installation. S 925 b) Clearance between propeller and aircraft structure. S 951 Fuel system - vapour locks. S 959 Unusable fuel..- S 967 Fuel tank installation. S 975 c) Fuel tan k vents. S 977 b) Fuel filter. S 993 e) Fuel lines. S 1145 Ignition switch. S 1301 Installed equipment. In addition, Inspectors must pay attention to the relevant "Spotlight" and Defect Warning reports in the BMAAInspectors' Manual. TAOS B""o-28 Page 6 of 8.

7 TADS BMO-28 Issue Appendix 1 2 TARJANI TRIKE

8 TYPHOON SINGLE PLACE WING Basic structure minimum standard: Leading edges: 1.75 inch 17g fi'l'301'f ~ith 1 metre long oversleeve, 17g., I 2 2. NtJ(.,1t1'\N r.l.1. P. Keel: 1.75 inch 18g HT30TF Cross tubes: 2 inch 17g HT30TF with 17g oversleeve of 1.16 metres each side Control frame uprights: inch 16g with 17g full length sleeve. Rigging wires minimum: Side wires: 3mm Remainder: 2.5mm.", If) / O~"'" &.f1j.! fn..z.v( 3 '\ " t' '... -1» 0 (j) ""0 OJ (Q <1> CD 0 -n NoM o.(}p OtJ-1 10 P1 OJ ~ 0 I ):>1\.) "0 CD "0 <1>... :J CJ) o...cj) ~.C: X <1>.