When.com Web Search

  1. Ads

    related to: ultralight aircraft engine options

Search results

  1. Results From The WOW.Com Content Network
  2. Phantom X1 - Wikipedia

    en.wikipedia.org/wiki/Phantom_X1

    Single seat ultralight aircraft with aerobatic capabilities, first flown in 1982. Standard engine is the 40 hp (30 kW) Rotax 447, with the 50 hp (37 kW) Rotax 503 or 64 hp (48 kW) Rotax 582 as options. In the USA the aircraft could be completed as a FAR Part 103 ultralight vehicle or as an Experimental amateur-built aircraft.

  3. Aero-Works Aerolite 103 - Wikipedia

    en.wikipedia.org/wiki/Aero-Works_Aerolite_103

    The Aero-Works Aerolite 103 is an American single seat, high-wing, pusher configuration ultralight aircraft, designed by Terry Raber and introduced by Aero-Works, Inc, of Millersburg, Ohio, in 1997. The aircraft's model number indicates that it was designed to comply with the Federal Aviation Administration FAR 103 ultralight rules. [1] [4] [5 ...

  4. Avid Flyer - Wikipedia

    en.wikipedia.org/wiki/Avid_Flyer

    The Avid Flyer is a family of American single engine, high-wing, strut-braced, conventional landing gear-equipped, two seat light aircraft designed for kit construction in the 1980s. Its several variants sold in large numbers. In 1987 a Flyer became the first ultralight to land at the North Pole. [citation needed]

  5. Ultralight aviation - Wikipedia

    en.wikipedia.org/wiki/Ultralight_aviation

    Huntair Pathfinder Mark 1 ultralight. Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons, elevator and rudder, calling the former "microlight" and the latter "ultralight".

  6. Flying K Sky Raider - Wikipedia

    en.wikipedia.org/wiki/Flying_K_Sky_Raider

    The power range is 28 to 50 hp (21 to 37 kW) and original standard engine specified was the 28 hp (21 kW) Rotax 277 with the 40 hp (30 kW) Rotax 447 as an optional, although the additional weight would probably put the aircraft in the US homebuilt category.

  7. Rans S-12 Airaile - Wikipedia

    en.wikipedia.org/wiki/Rans_S-12_Airaile

    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.