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This division offers two models, the Summit Steel Breeze two-place and the United States ultralight category FAR 103 Ultralight Vehicles compliant Summit 103 Mini Steel Breeze. As of 2012 Steel Breeze was a line marketed by Summit Aerosports Inc of Yale, Michigan. [9] [16] [17] [18] [19]
The Falcon was designed as a high-end, two-place ultralight trainer. It features a parachute-style high-wing, two seats in tandem or just a single seat, tricycle landing gear and a single 64 hp (48 kW) Rotax 582 liquid-cooled engine in pusher configuration as standard equipment. [1] [2]
The Robertson B1-RD is an American ultralight aircraft that was designed by Glen Bashforth and Bruce Bashforth and produced by the Robertson Aircraft Corporation. The aircraft was supplied as a kit for amateur construction with production starting in June 1982.
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.
Building on the success of the single-seat Beaver models, Spectrum Aircraft introduced the two-place Beaver RX 550 in December 1984. The fuselage was shown at an ultralight trade show in Los Angeles and test flown in February of 1985. It quickly became the most popular ultralight trainer in Canada.
Challenger I (Challenger UL) Single seat, 31.5 ft (9.6 m) wingspan gives lower stall speed. Can be fitted with a variety of engines. Qualifies as a US "Experimental - Amateur-Built", Light sport aircraft or with the 22 hp (16 kW) Hirth F-33 engine as a US FAR 103 Ultralight Vehicle, 800 reported completed and flown by the fall of 2011.
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