BRAND and MODEL
SEAHAWK CONDOR
TYPE
Two-seat light sport aircraft
ORIGIN
United States of America
ENGINE
(Condor III)
One 30 kw (40 hp) Kawasaki 440 two-cylinder, in-line, two-stroke converted snowmobile engine
SPECIFICATIONS
Wingspan: 9.8 m (32 ft)
Wing area: 15.6 m² (168 sq ft)
Never exceed speed: 97 km/h (60 mph)
Cruising speed: 89 km/h (55 mph)
Stalling speed: 31 km/h (19 mph)
Max glide ratio: 7:1
Rate of climb: 236 m/min (775 ft/min)
Wing loading: 15.8 kg/m² (3.24 lb/sq ft)
Fuel capacity: 19 litres (4.2 Imp gals)
Empty weight: 109 kg (240 lb)
Loaded weight: 247 kg (545 lb)
PHOTO
Flite Test:Source of phothograph
