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VS (stall speed): 35 kts | 40 mph | 65 kph
VC (cruise speed): 86 kts | 99 mph | 160 kph
VNE (never exceed speed) : 114 kts | 132 mph | 212 kph
Climb ratio: 1200 ft/min | 6 m/s
Glide ratio: 9

Takeoff distance over 50ft (15m) obstacle: 920 ft | 280 m
Landing distance over 50ft (15m) obstacle: 980 ft | 300 m

MEW (manufacturers empty weight): 260 kg | 573 lbs
MTOW (maximum takeoff weight): 450 kg | 992 lbs

Engine: UL260i
Fuel consumption: 11,5 litres/hour

The Mission M106 is now available as a factory built Microlight (ULM/UL) category aircraft with tailwheel or nosewheel. It is standard fitted with a state of the art UL260i engine and glass cockpit. For more info: www.lambert-aircraft.com


Price: 36900 EURO

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From the same manufacturer:

M106

Cruise speed: 85 kts
Empty weight: 260 kg | 573 lbs

M106 - Lambert Aircraft Engineering

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