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The Aeroprakt A-22 Foxbat is a Ukrainian two-seat, high-wing, tricycle landing gear ultralight aircraft that was designed by Yuri Yakovlev and is manufactured by Aeroprakt. In the United States the A-22 is referred to as the Valor, [2] while in the UK and Australia it is called the Foxbat. It has also been marketed as the Vision.
Taylor Bird 1980 2 seat homebuilt, unk no. built [21] Strojnik S-2 1980 motorglider 1 seater, 8+ built. Aérostructure Lutin 80 1983 1 seat ultralight motorglider, 2 built [22] Birdman Chinook 1982 ultralight homebuilt, 1100+ built; Alpha J-5 Marco 1983 1 seat ultralight motorglider, unk no. built [20] Quad City Challenger 1983 2 seat ...
The aircraft features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, tricycle landing gear with wheel pants and a single engine in pusher configuration. [1] The aircraft is made from bolted-together aluminum tubing, with its double surface wing covered in Dacron sailcloth.
The Aero Designs Pulsar is an American two-seat, low wing, ultralight and homebuilt aircraft that was designed by Mark Brown and first produced by Aero Designs of San Antonio, Texas, introduced in 1985. When it was available the Pulsar was supplied as a ready-to-fly aircraft and as a kitplane for amateur construction. [1] [2]
Data from Smithsonian General characteristics Capacity: 2 Length: 15 ft (4.6 m) Wingspan: 35 ft (11 m) Height: 10 ft (3.0 m) Empty weight: 310 lb (141 kg) Gross weight: 660 lb (299 kg) Powerplant: 1 × Cuyuna 430R air-cooled two-cylinder inline, 35 hp (26 kW) See also Ultraflight Lazair References Wikimedia Commons has media related to American Aerolights Double Eagle. ^ a b "American ...
Birdman Chinook 2S showing the pentagonal cockpit cross-section Birdman Chinook 2S Birdman Chinook 2S cockpit Birdman Chinook 2S Rotax 503 engine installation. The Birdman Chinook is a family of single and two-place, pusher configuration, high-wing ultralight aircraft that was first flown on 12 December 1982 and produced by Birdman Enterprises of Edmonton, Alberta, Canada, starting in 1983.
The aircraft replaces the Spyder's two-stroke engine with a Yuneec Power Drive 20 20 kW (27 hp) electric motor and two 28 lb (13 kg) Lithium polymer battery packs which provide a 40-minute endurance. The aircraft is intended to be developed into a commercially available kit and forecast to be available for under US$25,000.
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). The aircraft has a standard empty weight of 238 lb (108 kg). It features a cable-braced high wing, a single-seat open cockpit, tricycle landing gear and a single engine in pusher configuration. [1] [2]
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