|
The Cobra B was available as a kit from Advanced Aviation Inc. of
Orlando, Florida. It was developed from the earlier Advanced Aviation
Huski. The Cobra VIP was powered by a Rotax 447 and the Ag Cobra by a
Rotax 532. The two seat King Cobra B was first flown in 1983 and is
powered by a 65hp(48kW) Rotax 532 and has a range of 75miles(120km),
cruising speed of 55mph(88kmh), empty weight of 325lb(147kg) and a
maximum take-off weight of 775lb(351kg). Examples are still airworthy in
several countries.
Unregistered USA
Single seat ultralight first flown in 1982
Engine: 35hp(26kW) Rotax
377
Length: 17’11”(5.46m)
Height: 8’3”(2.51m)
Wingspan: 34’8”(10.57m)
No.built: 100+
Range: 90miles(145km)
Cruising speed: 45mph(72kmh) Empty weight: 252lb(114kg)
Maximum take-off weight: 525lb(238kg) |
AircraftWorldDirectory.com