The Seahawk Condor is an American ultralight aircraft that was designed by Buddy Head, Bob Carswell and Dave French and produced by Seahawk Industries and later by Condor Aircraft.
[1][2] The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).
It features a cable-braced high-wing, open cockpit, tricycle landing gear and a single engine in pusher configuration.
[1][2] The aircraft is made from bolted-together aluminum tubing, with the wings and tail surfaces covered in Dacron sailcloth.
The standard powerplant supplied was the Kawasaki 440 which produces 40 hp (30 kW).