BRITISH MICROLIGHT AIRCRAFT ASSOCIATION

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-28 ISSUE: 1

TYPE: TYPHOONJTARJANI TRIKE(G-MJCU - only example of type)

(1 ) MANUFACTURER: Wing: Solar Wings Ltd (UK)Trike: F. Tarjani (UK)

(2)

(3)

UK IMPORTER: NjA

CERTIFICATION BASIS: BCAR Section S requirements listed in CAA documentdated 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: .

15.4 m210.0 m1.54 m85 kg205 kg5.52 kgjm213.31 kgJm215 litres .

DOCUMENT.ISSUE STATUS

TAOS BMo-28 Page 1 of 8.

Issue RevisIOn Date Authorisation Pages Valid pages at thisNumber Reference affected Issue number 1

1 New 14.12.93

B tJlfJAll new Page No. Page Issue

HAAN1135 . \ }I - " ,'" ...

1 12 13 14 15 16 17 18 1

MICROLIGHTTYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-28 ISSUE: 1

(6) PQWERPLANTS

.

~Qi5e reQuirement:

- 1 SeatReGistered Pre 1/4/86 80 dBA

~eGistered Post 1/4/86 76 dBA

2 Seat

~lliLdBA

BCAR Reference

N3-6. 3 Iss 4

1Ij:l~6. 4 I s s 4-

TAOS 8M0-28 Page 2 of 8.

Designation Typhoon/Tar] aniTri ke

Engine Type Fuji RobinEC25PS. Invtd

Reduction 2.32:1Gear/ratio

Exhaust Nicklow '

System

Intake -System

Propeller LaminatedType wood

,

Propeller 52" x 28"Dia x Pitch

Noise Type 108MCert. No. Issue 1

Designation"

Engine Type

ReductionGear/ratio

ExhaustSystem

Intake ,System \

PropellerType

PropellerDi a x Pitch

Noise TypeCert. No.

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-28 ISSUE: 1

*(a)

MANDATORYLIMITATIONS~ (* indicates which are placarded)(7)

*(b)

(c)

*(d)

(e)

(f)

*(g)

Max Take-off Weight: 205 kg

C G Limits: N/A - weightshift

C G Datum:

Cockpit Loadings

Pilot or Ballast (min)

Pilot or Ballast (max)

Permanent Ballast, Weight and Position: Not fitted.

Empty C G:

Never Exceed Speed: 55 mph

*(i)

*~~h) y Manoeuvring Speed: 55 mph

*(j)

(k),

Manoeuvre Limitatio~s: Aerobatics prohibited. Roll <600 ban kPitch <+/- 30°

Fuel Contents (Max Usable): 15 litres .Power Plant: See Table below

TADS BMo-28 Page 3 of 8.

Front Rear Total

55 kg - kg 55 kg

90 kg - kg 90 kg

ENGINE Fuj i Robi nEC25PS

Max RPM 6500

Max CHT N/A

Max EGT N/A

Fuel Spec 92 Oct (mln)Petrol/oil

Engine Self mi xOil Soec 2 strokeGearbox N/AOil Soec \

Fuel/Oil Mix 40:1

Oil Pressure N/A

Oil Temp N/A

Coolant Temp N/A

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-28 ISSUE: 1

(8) INSTRUMENTS REQUIRED FOR TYPE ACCEPTANCE:

Compass EGT Coolant TemQ

NjA NjA NjA

(9) CONTROL DEFLECTIONS (3-AXIS SYSTEMS): NjA - weightshift

Pitch ControlTailplane TrimAileronsRudderSteerinoSpoilers

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 MAXT/0 WEIGHT:

Rate of Climb:~

300 ftj min ute

Stall or Minimum Flying Speed: 28 mph

TAOS BMD-28 Page 4 of 8.

ASI Altimeter RPM CHT

Required Req ui red Req ui red NjA0 to >55 mph Wrist type

or equivalent acceptable

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-28 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.

IssueAutho:r:isation

Date BMAA

/ 3!tIR/l I'f- ,2J~~~4r 9r~

f- "

".,

BLANKIS4.TAD

TAOS BMO-28 Page 5 of 8.

MICROLIGHT TYPE ACCEPTANCEDATA SHEET (TADS)

NO: BMO-28 ISSUE: 1

APPENDIX 1.

ADDITIONAL DOCUMENTATION

The Typhoon/Tarjani Tri ke must satisfy the modification and inspection provisions setout 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 1303 1) Airspeed indicator.

. S 1303 2)Altimeter placard (where applicable).S 1541 pthe,r placards.

b) InsQection:

S 603S 605S 607S 609S 623S 626S 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 DefectWarning reports in the BMAAInspectors' Manual.

TAOS B""o-28 Page 6 of 8.

TADS BMO-28 Issue

Appendix

1

2

TARJANI TRIKE

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

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CD

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Cross tubes: 2 inch 17g HT30TFwith 17g oversleeve of 1.16 metres each side

Control frameuprights: 1.125 inch 16g

with 17g full length sleeve.

Rigging wires minimum:Side wires: 3mmRemainder: 2.5mm

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