Ultralight Aircraft Database | Pilotmix
38 pilots online!
Browse manufacturers

VS (stall speed): 22 kts | 25 mph | 40 kph
VC (cruise speed): 30 kts | 35 mph | 56 kph
VNE (never exceed speed) : 56 kts | 65 mph | 105 kph

MEW (manufacturers empty weight): 106 kg | 234 lbs
MTOW (maximum takeoff weight): 215 kg | 475 lbs

Engine: Kawasaki 440

The Condor is a single seat, high wing, wire braced ultralight, featuring a tri-cycle landing gear suspension system.

The control system is conventional stick and rudder, with spoilerons on the wings for aiding in roll control.

The plane is has a single surface wing, and is wire braced. The kit came as a simple bolt together assembly taking approximately 75 hours to assemble.

The Condor single was powered by Kawasaki 440 engines, with some of the two seaters equipped with Kawasaki liquid cooled engines of 80 hp.

The Condor single place and two place were produced up until about 1984.

Photo and text from: http://www.ultralightnews.com/antulbg/condor_ultralight.htm


Share this aircraft!
ULTRALIGT CLASSIFIEDSUltralight classifieds

TWITTERUltralight classifieds

OTHER USERS ARE NOW BROWSING...Other users are now browsing...