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The Colibri V/STOL light aircraft has been developed
by Duncan Aviation Inc. of Fenton, Michigan as an alternative to
traditional runway dependent aircraft. Kits were to be made available to
homebuilders although the current status of the project is unknown at
this time.
N44CX
c/n 001
USA
4 seat light aircraft first flown in 1999
Engines: 4X 125hp(93kW) Hirth F.90
Length: 18’0"(5.48m)*
Height: 11’0"(3.35m)* Wingspan: 20’0"(6.09m)*
No.built: 1+ Range: 800miles(1284km)
Cruising speed: 280mph(449kmh) Empty weight: 1500lb(680kg)
Maximum take-off weight: 3000lb(1361kg) |
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