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M108 general spe - 4 Pages

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M108 general spe
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Catalogue excerpts

LAMBERT AIRCRAFT ENGINEERING

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Mission M108 Description Wings Fabric covered wings supported by wing struts. Dual tubular aluminium alloy wing spars. Plywood wing ribs. Frise ailerons operated through cables. Manually operated trailing edge flaps. Quick wing folding system. Fuselage Fabric covered welded space frame fuselage structure from high strength steel alloy tubing. Horizontal tailplane supported by streamlined struts. Fixed fin with conventional rudder. Landing gear Fuselage mounted fixed landing gear. Main landing gear legs by cantilever composite leaf springs. 6” main wheels with hydraulic disc brakes. Different tyre...

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Mission M108 Equipment & Options Landing gear and brakes Manual brake lever Parking brake valve Toe brakes on pilot side Toe brakes on passenger side Main wheel tyres 15x6.00x6, nose wheel tyre 4.00x6 All tyres 8.00x6 (Carlisle) Tyres 26”x12”x6” (Alaskan bush tyres) Wheel spats Exterior Exterior trim, standard trim scheme in 2 colours of choice Aircraft exterior colour in other colour than white Full custom paint scheme Tinted windshield and windows (with anti-UV and IR coating) Full transparent doors Interior & Safety Equipment Four point seat harnesses (Schroth), TSO Airframe emergency recovery...

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Mission M108 Specifications Wing span Wing area Aspect ratio Tailplane span Length Height Wheel track Width with wings folded Baggage capacity Cabin width Fuel capacity, standard Fuel capacity, optional Never exceed speed Max. crosswind comp. Limit load factors 31 ft 4 in (9.57 m) 131 sq ft (12.2 m²) 7.45 7 ft 11 in (2.40 m) 20 ft 0 in (6.10 m) 7 ft 6 in (2.25 m) nosewheel 6 ft 2 in (1.90 m) taildragger 5 ft 11 in (1.77 m) 8 ft 6 in (2.60 m) 90 lbs (40 kg) 43 in (1.08 m) 20.5 US gal (78 litres) 29.0 US gal (110 litres) 120 kt (222 km/h) 12 kt (22 km/h) taildragger 16 kt (30 km/h) nosewheel +3.8/-1.9...

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