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MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS) NO BMO-42 ISSUE: 6 GEMINI SPRINT -X, TRlFL YER SPRINT -X. PUMA SPRINT-X, SPRINT TRlFL YER 440 (1) MANUFACTURER: Mainair Sports Ltd, Rochdale, Lancs Southdown Sai1wings(no longer trading) Sprint Wing & Puma Trike components available from Medway Microlights, Rochester, Kent. British Micro1ightAircraft Association is now responsible for continued airworthiness. (2) (3) UK IMPORTER: N/A CERTIFICATION BASIS: BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18dated 17/1/86 (type acceptance). (4) DEFINITION OF BASIC STANDARDS: Mainair Sports 440 Dual Master list of Drawings Issue 2 dated 16.5.84. Southdown Sai1wings 1000 issue A drawings schedule. (5) DIMENSIONSIWEIGHTFOR COMPLIANCE WITH MICROLIGHT DEFINITION (a) Wing Area (b) Span (c) Standard Mean Chord (d) Dry Empty Weight (e) Max Takeoff Weight (f) Empty Wing Loading (g) Wing loading (max AUW) 16.73 m2 (180 ft2) 10.67 m (35 ft) 1.56 m (5.1 ft) 145kg 338kg 8.52 kg/m2 20.2 kg/m2 ~ Page 1 of 5

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18 dated 17/1/86 (type acceptance). (4)

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Page 1: MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18 dated 17/1/86 (type acceptance). (4)

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO BMO-42 ISSUE: 6

GEMINI SPRINT -X, TRlFL YER SPRINT -X. PUMA SPRINT-X, SPRINT TRlFL YER 440

(1) MANUFACTURER: Mainair Sports Ltd, Rochdale, LancsSouthdown Sai1wings(no longer trading)

Sprint Wing & Puma Trike components availablefrom Medway Microlights, Rochester, Kent.

British Micro1ightAircraft Association is nowresponsible for continued airworthiness.

(2)

(3)

UK IMPORTER: N/A

CERTIFICATIONBASIS:

BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAAletter 9/301UL18dated 17/1/86 (type acceptance).

(4) DEFINITION OF BASIC STANDARDS:

Mainair Sports 440 Dual Master list of Drawings Issue 2 dated 16.5.84.Southdown Sai1wings1000 issue A drawings schedule.

(5) DIMENSIONSIWEIGHTFOR COMPLIANCE WITH MICROLIGHT DEFINITION

(a) Wing Area(b) Span(c) StandardMean Chord(d) Dry Empty Weight(e) Max Takeoff Weight(f) Empty Wing Loading(g) Wing loading (max AUW)

16.73 m2 (180 ft2)10.67 m (35 ft)1.56 m (5.1 ft)145kg338kg8.52 kg/m220.2 kg/m2

~

Page 1 of 5

Page 2: MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18 dated 17/1/86 (type acceptance). (4)

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO BMO-42 ISSUE: 6

Page 2 of 5

6) POWER PLANTS

440 Dual 440 Dual 440 Dual 440 Dual (4) not used

Designation (1) (2) (3)

Fuji Robin Fuji Fuji Fuji RobinEngine Type EC 44PM Robin EC Robin EC EC 44PM

44PM 44PM

Reduction Gear 2.61:1 2.67:1 2.67:1 2.8:1Nicklow

Exhaust System Nicklow Rota Flow Rota Flow NicklowMuffler Muffler

Intake System - - - -

Propeller Type Mainair Mainair Mainair 2 blade

, Round tip wood

Propeller rl)ia,.x 62" x 30" 62"x27.5" 62"x30" 62" x 37"

Pitch'

Noise Type Cert 5m Issue 1 2M 2M Iss. 3 1m Iss. 3No.

Puma Puma Puma Puma PumaDesignation SprintX (1) SprintX (2) SprintX (3) SprintX (4) SprintX (5)

Fuji Robin Fuji Robin Fuji Robin Fuji Robin Fuji RobinEngine Type EC44PM EC44PM EC44PM / EC44PM / EC44PM

EC442PM EC442PM Upright

Reduction Gear 2.6:1 2.6:1 2.67:1 2.61: 1 2.5:1

. Nicklow

Exhaust System Rotaflow Rotaflow Rota Flow Nicklow NicklowMuffler

Intake System - - - - ,-

Propeller Type 2 blade 2 blade Mainair Nicklow 2 blade

wood wood wood

Propeller Dia x 60" x 32" 62"x32" 62"x27" 58"x36" 60" x 32"Pitch

Noise Type Cert 1M iss 3 1M issue 3 1M Iss. 2 1M Iss. 2 1M issue 4No.

Page 3: MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18 dated 17/1/86 (type acceptance). (4)

Page 3 of 5

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO BMO-42 ISSUE: 6

(7) MANDATORY LIMITATIONS: (*to be placarded)

(A) Max Take-off Weight: 338 kg *

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

(C) C G Datum ilia

(D) Cockpit Loadings: Front Rear Total *

Pilot and Baggage or Ballast (Min) 55kg 15kg 70kgPilot and Baggage (Max) 90kg 90kg 180kg

(E) Empty Weight (nominal): 143 kg

(F) Empty C of G (3-Axis Aircraft): nil

(GY' N:ever Exceed Speed: 51 knots *

(H) Manoeuvring Speed: 38 knots *

(I) Permitted Manoeuvres: Non Aerobatic. *

(J) Fuel Contents (Max Useable): 22 litres *

(K) Power Plant: * See Table below:-

Engine Fuji Robin EC44PM - all variants

Max RPM 6900

MAX CHT 218 °C

Fuel Spec 92RON minimum Petroleum Spirit

Oil Spec SELF MIX 2 STROKE

Fuel/Oil Mix 40:1

Max EGT 815°C

Oil Press N/A

Oil Temp N/A

Page 4: MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18 dated 17/1/86 (type acceptance). (4)

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO BMO-42 ISSUE: 6

(8) INSTRUMENTSREQUIRED FOR TYPE ACCEPTANCE:

(9) CONTROL DEFLEECTIONS (3-Axis Systems):

N/A

(10) PILOT'S NOTES, MAINTENANCE MANUALS REFERENCES:

Operation and Maintenance Manuals for Gemini/Triflyer Sprint, and Striker Gemini/TriflyerDoc. REF TOM-I-440 Dual.

( "

(11) MANDATORY MODIFICATIONS / SERVICE BULLETINS / AIRWORTHINESSDIRECTIVES ETC:

See BMAA Documents: TSO04Issue 2 (Triflyer and Gemini trikes)TSOOIIssue 3WSOOIIssue 1 (Sprint Wing.)Also BMAA MAAN 1170

(12) MINIMUM PERFORMANCE AT MAX TAKE-OFF WEIGHT

Rate of climb: 355 [pm

Stall or Minimum flying speed: ~ 48 kph

G B GrattonChief Technical Officer

14 December 1998,

Page 4 of 5

ASI Altimeter RPM CHT Compass EGT

Required Required

Page 5: MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)BCAR section S advance issue 1983, selecting the agreed paragraphs according to CAA letter 9/301UL18 dated 17/1/86 (type acceptance). (4)

MICROLIGHT TYPE ACCEPTANCE DATA SHEET (TADS)

NO BMO-42 ISSUE: 6

Issue History

Illustration of Typical Aircraft (Puma Sprint-X) .

Page 5 of 5

Reference Date Authorisation Affected Validpages

pages

Issue 1 MAAN 1170 issue 1 27/4/1998 W G Brooks All 1 to 4CTO BMAA New

Issue 2 MAAN 1170 issue 2 18/5/1998 W G Brooks 1&3 1 to 4CTO BMAA

Issue 3 62" x 37" propeller 18/8/94 W G Brooks 2 1 to 5CTO BMAA

Issue 4 62" x 32" propeller 29/5/95 W G Brooks 2 1 to 5CTO BMAA

Issue 5 60" x 32" propeller for Puma Sprint X 12/3/96 W G Brooks 1,2 1 to 5CTO BMAA

Issue 6 Reclassify two Puma Sprint configurations 14/12/98 G B Gratton all 1 to 5

as Puma Sprint X (3) and (4) CTO BMAAf- ,. - Ne,,:,Puma Sprint X (5) based upon

G-MJCE .