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Lambert Aircraft Engineering Mission M108


The Mission M108 Light Sport Aircraft is a two seater single engine light sport aircraft. It has an unswept untapered high wing. The fuselage provides comfortable side-by-side seating. Two upwards hinging doors provide access to the cabin. The large transparent areas of the cabin provide excellent visibility in level flight as well as in turns. Both seats are individually adjustable. Elevator and aileron control is by sticks. The aircraft is standard equipped with full dual controls.

The fuselage is a welded space frame, which is fabric covered. High strength steel tubing is used throughout. The wings are of aluminium construction and also fabric covered.
Control surfaces are conventional with single slotted flaps, pushrod operated elevator and cable operated rudder and ailerons. The main landing gear consists of composite cantilever leaf springs. The Mission M108 is available as either a tailwheel or a nosewheel version.

The front mounted ULPower UL260i engine produces 85 HP at 2850 rpm and drives a three blade ground adjustable propeller. The four stroke four cylinder engine is air cooled and features FADEC (Full Authority Digital Engine Control).

With a large choice of options, instruments and avionics, your Mission M108 can be customised to meet your personal preferences.
Depending on the applicable national regulations, the Mission M108 is available as a kit built aircraft or as a ready to fly factory built aircraft.

Mission M108
Engine: ULPower UL260I, 62 kW (85 HP) at 2850 rpm
Wing span: 9.32 m (30 ft 6 in)
Wing area: 11.8 sq.m (127 sq.ft)
Aspect ratio: 7.4     
Length:     6.10 m (20 ft)
Height TD: 2.15 m (7 ft 1 in)
Height NW: 1.95 m (6 ft 6 in)
Width wings folded: 2.60 m (8 ft 7 in)
Wheeltrack: 1.75 m (5 ft 10 in)
Max. all up weight: 1320 lbs (600 kg))     
Empty weight: 680-700 lbs (310-320 kg)     
Fuel capacity: 78 lt standard
Fuel capacity: 110 lt long range
Baggage capacity: 40 kg (90 lbs)
Never exceed speed: 112 kt (210 km/h )     
Max. level speed at S/L: 100 kt (185 km/h)     
Max. S/L rate of climb: 850 ft/min (4.25 m/s)     
Cruise speed: 80-85 kt (150-160 km/h)     
Fuel consumption: 12-15 litres/h     
Range (20 min res.): 460 nm (850 km)     
Stall speed, full flaps: 39 kts (72 km/h)     
T-O ground roll: 80-110 m     
Max. crosswind TD: 12 kt
Max. crosswind NW: 16 kt
Limit load factors: +3.8/-1.9
Tailplane span: 2.40 m (8 ft 0 in)
Cabin width: 1.08 m (43 in)

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