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  2. Ultralight aircraft (United States) - Wikipedia

    en.wikipedia.org/wiki/Ultralight_aircraft_(United...

    Ultralight aircraft exist outside of the United States. In most countries, ultralights are a class of aircraft. A completely different legal concept is valid within the USA. The FAA makes explicitly clear that ultralight vehicles are not aircraft, are not regulated as aircraft, and are exempt from aircraft rules.

  3. Sadler Vampire - Wikipedia

    en.wikipedia.org/wiki/Sadler_Vampire

    The Sadler SV-1 Vampire is a single-seat ultralight sport aircraft developed in the United States in the early 1980s. [1] It is uncharacteristic of ultralight designs in both its layout and its construction. The Vampire is a mid-wing cantilever monoplane of pod-and-boom configuration and twin booms joined by a common horizontal stabilizer. [1]

  4. 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.

  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. ICP Savannah - Wikipedia

    en.wikipedia.org/wiki/ICP_Savannah

    Data from Jane's All the World's Aircraft 2010/11 General characteristics Crew: 2 Length: 6.60 m (21 ft 8 in) Wingspan: 9.00 m (29 ft 6 in) Height: 2.58 m (8 ft 6 in) with optional rudder extension 2.88 m (9 ft 5 in) Wing area: 12.87 m 2 (138.5 sq ft) gross Airfoil: NACA 65-018 (modified) Empty weight: 286 kg (631 lb) Max takeoff weight: 450 kg (992 lb) European ultralight; experimental 560 kg ...

  7. Pivotal BlackFly - Wikipedia

    en.wikipedia.org/wiki/Pivotal_BlackFly

    By September 2017, the prototype had flown 10,000 mi (16,093 km) in a series of flights of at least 30 mi (48 km) each. The first pre-production aircraft was flown in October 2017. [1] [5] The design is intended for the FAR 103 Ultralight Vehicles category in the United States and the Basic Ultralight Aeroplane category in Canada. The American ...