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  2. Light-sport aircraft - Wikipedia

    en.wikipedia.org/wiki/Light-sport_aircraft

    The civil aviation authorities in different countries have their own particular specifications and regulations which define the LSA category.. For example, in Australia the Civil Aviation Safety Authority defines a light-sport aircraft as a heavier-than-air or lighter-than-air craft, other than a helicopter, with a maximum gross takeoff weight of not more than 560 kg (1,235 lb) for lighter ...

  3. Flying K Sky Raider - Wikipedia

    en.wikipedia.org/wiki/Flying_K_Sky_Raider

    First flown in 1996, the original Sky Raider is a single seater designed as an FAR 103 Ultralight Vehicles compliant aircraft with an empty weight within that category's 254 lb (115 kg) empty weight limit, when equipped with a light enough engine.

  4. Flaeming Air FA 04 Peregrine - Wikipedia

    en.wikipedia.org/wiki/Flaeming_Air_FA_04_Peregrine

    The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules, with different models for each category. It features a cantilever low-wing , a two-seats-in- side-by-side configuration enclosed cockpit under a bubble canopy , fixed tricycle landing gear , or optionally ...

  5. Tecnam P2002 Sierra - Wikipedia

    en.wikipedia.org/wiki/Tecnam_P2002_Sierra

    The Tecnam P2002 Sierra is a two-seat, low-wing, light aircraft. [2] A major market for the Sierra is the flight training sector; accordingly, its design and several of its major features, such as the use of a low-mounted wing and a bubble canopy, result in the aircraft being particularly well-suited to use as a trainer.

  6. Quad City Challenger - Wikipedia

    en.wikipedia.org/wiki/Quad_City_Challenger

    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.

  7. Zenith STOL CH 701 - Wikipedia

    en.wikipedia.org/wiki/Zenith_STOL_CH_701

    A Zenith STOL CH 701 on wheels A Czech Aircraft Works-built CH 701 AMD-built CH 750 CH 750 CH 750 instrument panel CH 701 Turboprop CH 701 Turboprop in flight. The Zenith STOL CH 701 and CH 750 are a family of light, two-place kit-built STOL aircraft designed by Canadian aeronautical engineer Chris Heintz through his Midland, Ontario, based company, Zenair.

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