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Unusually for this period in aircraft history when most ultralights had two-axis control, the Ultrastar has standard three-axis controls, including full span ailerons. [ 1 ] When the original Flyer was designed there were no suitable lightweight engines available, so the Flyer first fitted two Chrysler powerplants and later two 11.5 hp (9 kW ...
The US Light Aircraft Hornet is an American two-seats-in-tandem, pusher configuration, tricycle gear, strut-braced high wing ultralight aircraft, that was produced US Light Aircraft Corporation of Ramona, California between 1994 and circa 2008 in kit form for amateur construction. It was also available as a factory-completed light-sport aircraft.
In 1992 Spectrum Aircraft of Surrey, British Columbia, the manufacturer of the Spectrum Beaver aircraft line, went out of business and the following year ASAP began making parts for the existing RX-28, RX-35 and RX-550 Beaver fleet. In 1996, after a similar development program to the Chinook Plus 2, ASAP introduced an improved two-seat Beaver ...
The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in doped aircraft fabric. Its 33.00 ft (10.1 m) span wing has a wing area of 220.0 sq ft (20.44 m 2). The Hornet has the largest wing area and lightest wing loading of any ultralight of its period.
Regulation of ultralight aircraft in the United States is covered by the Code of Federal Regulations, Title 14 (Federal Aviation Regulations), Part 103, or 14 CFR Part 103, which defines an "ultralight" as a vehicle that: has only one seat [1] [2] Is used only for recreational or sport flying [1] [2]
The Weedhopper is an American high-wing, tractor configuration, tricycle gear, two-axis control ultralight aircraft originally developed by John Chotia during the height of the 1970s ultralight boom and introduced in 1977. When it was in production the aircraft was sold as a kit for amateur construction and could be assembled in 25-30 man-hours.
Mitchell later modified the design into a powered ultralight aircraft with wheeled tricycle landing gear, known as the B-10. The B-10F is a foot-launched variant with only two wheels. [2] The B-10 was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft ...
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".
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