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  2. Birdman Chinook - Wikipedia

    en.wikipedia.org/wiki/Birdman_Chinook

    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.

  3. Aircraft Sales and Parts - Wikipedia

    en.wikipedia.org/wiki/Aircraft_Sales_and_Parts

    ASAP Chinook Plus 2 ASAP Beaver RX-550 ASAP Beaver SS at the Canadian Aviation Expo Summit II powered parachute. Aircraft Sales and Parts (ASAP) is an American kit aircraft and parts manufacturer, founded in Vernon, British Columbia and moved to Sealy, Texas in 2013 and renamed the Aeroplane Manufactory.

  4. Birdman Enterprises - Wikipedia

    en.wikipedia.org/wiki/Birdman_Enterprises

    Birdman MJ-5 hang glider Birdman MJ-5 hang glider Birdman Chinook 2S Birdman Chinook 2S. Birdman Enterprises Limited was a Canadian aircraft manufacturer that commenced business in 1973 and became well known for its line of hang gliders and later its ultralight aircraft until its demise in late 1987. [2] [3] [4]

  5. Spectrum Beaver - Wikipedia

    en.wikipedia.org/wiki/Spectrum_Beaver

    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. The combination of its predictable and docile handling, along with the reliable Rotax 503 50 hp (37 kW) engine, ensured its success. Larry Croome left Spectrum Aircraft Inc in 1986.

  6. Buzzman L'il Buzzard - Wikipedia

    en.wikipedia.org/wiki/Buzzman_L'il_Buzzard

    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 ...

  7. Birdman Atlas - Wikipedia

    en.wikipedia.org/wiki/Birdman_Atlas

    Non-foot-launchable single place ultralight powered by a 20 hp (15 kW) 215 cc single cylinder Cuyuna 215 engine. Conventional three-axis control system utilizing spoilers for roll-control. Seat is adjustable fore and aft for balance. Due to company concerns about rigging requirements it was only supplied as a completed aircraft. [3] Atlas 250 3-A

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