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Challenger II on skis Challenger II landing on skis Challenger I single seat ultralight. The Quad City Challenger is a family of one and two seats-in-tandem, pusher configuration, tricycle landing gear ultralight aircraft that is designed and produced by Quad City Aircraft Corporation of Moline, Illinois. The Challenger was first introduced in ...
The aircraft in the background is a Quad City Challenger II. The Pterodactyl Ascender is a family of U.S. designed and built ultralight aircraft that were sold in kit form between 1979 and 1984 under Pterodactyl Limited and is currently being sold by DFE Ultralights.
The Excalibur was designed as "clone" [1] of the Quad City Challenger II aircraft. The company took the basic Challenger design and incorporated many changes, including mounting the engine upright allowing larger propellers and the Rotax gearbox to be mounted, lengthening the tailboom and enlarging the tail vertical surface to increase stability, shortening the ailerons and replacing control ...
The US Light Aircraft Hornet is an American two-seats-in-tandem, pusher configuration, tricycle gear, strut-braced high wing ultralight aircraft, that was produced US Light Aircraft Corporation of Ramona, California between 1994 and circa 2008 in kit form for amateur construction. It was also available as a factory-completed light-sport aircraft.
Quad City Challenger 1983 2 seat ultralight, 3,000+ built; Spectrum Beaver 1983 ultralight homebuilt, 2080+ built; Funk Fk6 1985 1 seat ultralight motorglider, unk no. built [23] Advanced Aeromarine Buccaneer 1988 2 seat amphibious biplane, unk no. built; D-8 Moby Dick 1988 2 seater, 37 built; Seabird Seeker 1989 observation aircraft 2 seater ...
Open-cockpit, conventional landing gear, ultralight trainer with two seats in tandem, standard engine is the Rotax 503 of 50 hp (37 kW) with the Rotax 582 of 64 hp (48 kW), 80 hp (60 kW) or the Rotax 912UL of 100 hp (75 kW) optional. The aircraft uses the wings, tailboom and tail of the S-12XL, but is fitted with a new steel tube cockpit structure.
Data from Cliche and L'il Hustler General characteristics Crew: one Capacity: one passenger Length: 20 ft 6 in (6.25 m) Wingspan: 33 ft 6 in (10.21 m) Wing area: 172 sq ft (16.0 m 2) Empty weight: 500 lb (227 kg) Gross weight: 1,200 lb (544 kg) in the Canadian basic ultralight category, 1500 lbs in the amateur-built category. Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 ...
The prototype was powered by a Rotax 277. Heavier engines can be installed, although the aircraft will not then meet the US FAR 103 weight requirements as an ultralight aircraft. Other engines used include the 40 hp (30 kW) Rotax 447, 35 hp (26 kW) Rotax 377, 30 hp (22 kW) 1/2 VW and the 22 hp (16 kW) Hirth F-33. [1] [2] [3] [4]
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