Mission M106 Light Aircraft

by Lambert Aircraft Engineering
3
7
Mission M106 Light Aircraft - Photo #1

The Mission M106 is now available as a factory built Microlight (ULM/UL) category light aircraft with tailwheel or nose-wheel. It is standard fitted with a state of the art UL260i engine and glass cockpit.

For more info: www.lambert-aircraft.com

Specifications

Empty weight:
573 lbs (260 kg)
MTOW:
992 lbs (450 kg)
Stall speed:
35 kts (40 mph) (65 kph)
Cruise speed:
86 kts (99 mph) (159 kph)
VNE:
114 kts (131 mph) (211 kph)
Climb:
1181 ft/min (6 m/s)
Glide ratio:
9
Take-off distance:
919 ft (280 m)
Landing distance:
984 ft (300 m)
Engine:
UL260i
Fuel consumption:
3 GPH (11.4 LPH)
For sale for: USD 47,472 / EUR 40,351

PHOTOS

Mission M106 Light Aircraft - Photo #2

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