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Mission M106 Lambert Aircraft Engineering

Mission M106
Mission M106

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3.5/5 rating (4 votes)

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

Specifications

  • Empty weight: 573 lbs
  • MTOW: 992 lbs
  • Stall speed: 35 kts
  • Cruise speed: 86 kts
  • Never exceed speed VNE: 114 kts
  • Climb: 1181 ft/min
  • Glide ratio: 9:1
  • Takeoff distance (50ft obstacle): 919 ft
  • Landing distance (50´ft obstacle): 984 ft
  • Engine: UL260i
  • Fuel consumption: 3 gph
  • Mission M106
  • For sale for: 47472 USD
(i) Switch to metric system.

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