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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".
It was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. The company name was later changed to Fisher Flying Products and production continued under that company name until the FP-101 was supplanted in production by the Fisher FP-202 Koala. [1]
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 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 ...
The FP-303 was designed by Fisher Aircraft in the United States in 1982 and was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. The design goal was to provide ultralight pilots with an aircraft that was as portable as possible.
The FP-202 was designed by Fisher Aircraft in the United States in 1981 and was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. It is also a 51% approved kit for the US homebuilt aircraft category.
The Avenger was designed to meet the requirements of the United States FAR 103 Ultralight Vehicles regulations, including the maximum 254 lb (115 kg) empty weight. Design goals included low cost, an attractive appearance, and accommodation for a 76 in (193 cm) tall, 240 lb (109 kg) pilot.
The aircraft has a 22:1 glide ratio. The FLAC has laminated fiberglass main landing gear legs and a nose wheel that is steerable. The aircraft was also designed to be at least nominally foot-launchable to comply with the informal US requirements for ultralights of that period that they be able to do so.