microlight type acceptance data sheet (tads) no: bmo … · (h) fuel capacity: excluding...

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO: BMO-50 ISSUE: 1

TYPE NIMROD/TRIFLYER

(1) MANUFACTURER: WING: AIRWAVE GLIDERS LTD, Cowes, Isleof Wight, U.K.

TRIKE: Mainair Sports, Rochdale, U.K.

(2)

(3)

UK IMPORTER: N/ A

CERTIFICATION BASIS: BCAR Section S requirements listed in CAA document

dated 17th January 1986, ref: 9/30/UL1B

DEFINITION OF BASIC STANDARDS: As defined by MAAN 1198 and this TADS.(4)

(5) DIMENSIONS/WEIGHT FOR COMPLIANCE WITH MICROLIGHT DEFINITION-

(a) Wing area (inc canard area,(b) Span:

(c) Standard Mean Chord:

(~) Dry Empty Weight:(e) Max Take-Off Weight:

(f) Wing Loading (Weight Empty/Wing Area):

(g) Wing Loading (Max Take-Off Weight/Wing(h) Fuel Capacity:

excluding winglets):15.8m210m1.58m80kg

190kg 25 kg/m12 kg/m2 .

20 lit resArea) :

(6) POWER PLANTS

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NIMROD/Designation TRIFLYER

FujiEngine Type Robin

EC25psINVERTED

Reduction 2.3:1 31Gear

Exhaust Rotaflow

System,

Intake System-

Propeller Mainair

Type

Propeller Dia 54"x27"x Pitch

Noise Type 75M issue

Cert No. 1

MICROLIGHT TYPE ACCEPTANCEDATA SHEET (TADS)

NO BMO-50 ISSUE: 1

(7) MANDATORY LIMITATIONS: * To be placarded

Max Take-off Weight: 190kg *

(C)

(D)

(E)

(F)

(G)f

(H)

(I)

(J)

(K)

U Oil Temp

(A)

(B) C G Limits (3-Axis Aircraft): NJA

C G Datum: N/A

Cockpit Loadings: Front Rear Total

Pilot and Baggage or Ballast (Min) 55kg

90kg

0 55kg *

0 90kg *Pilot and Baggage (Max)

Permanent Ballast, Weight and Position: None

Empty C of G (3-Axis Aircraft): NJA

Never Exceed Speed: 52 knots (60mph) *

.Manoeuvring Speed: 38 knots (44mph) *

Permitted Manoeuvres: Non Aerobatic Pitch <+ 300 *Roll <600 *

Fuel Contents (Max Useable): 20 litres

Power Plant See Table

-_1-.

of-4H

Engine Fuji RobinEC25PS

Max RPM 7000

MAX CRT

Fuel Spec B3MON or90 RONmin.

Petrol/Oil '

Oil Spec Self Mix2 Stroke

Fuel/Oil 40:1Mix

Max EGT

Oil Press

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO BMO-50 ISSUE: 1

(B) INSTRUMENTS REQUIRED FOR TYPE ACCEPTANCE:

EGT Coolant Temp

Pitch Control Up:- Down:-

Tailplane Trim Up:- Down:-

Ailerons Up:- Down: -

Rudder Left: - Right:-

f "'.Steenng Left:- Right:-

Spoilers

(10) PILOT'S NOTES, MAINTENANCEMANUALSREFERENCES:

Fuji Robin EC25PS manual.

Airwave Magic 1 owners manual, Nimrod Airframe drawings.

Maintain to BMAA schedule MMS issue 1.

(11) MANDATORYMODIFICATIONS/SERVICE BULLETINS/AIRWORTHINESS DIRECTIVES ECT:

As defined by MAAN IlB6~and MAAN 119B (Nimrod Wing).

(12) MINIMUMPERFORMANCEAT MAX TAKE-OFF WEIGHT

Rate of Climb: 300 ft/min (Using Fuji Robin EC25PS Engine).

Climb Speed: 26knots (30mphr

Stall or Minimum Flying Speed: 19knots (22mph)

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ASI Altimeter RPM CHT Compass

Reg Reg0-60mph Wrist Type

Acceptable

(9) CONTROLDEFLEECTIONS (3-Axis Systems): N/A

Notes

1.

MICROLIGHT TYPE ACCEPTANCEDATA SHEET (TADS)

NO HMO-50 ISSUE:!

G A Drawings and/or photographs illustrating the principal features ofthe aircraft submitted for type approval shall be attached to, and form

part of, this Data Sheet.

Issue Date ~ "i ::;k1 1/9/?It

"

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microlight type acceptance data sheet (tads) no: bmo … · (h) fuel capacity: excluding...

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