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An ultralight trike or paratrike is a type of powered hang ... Administration (FAA) as weight-shift-control aircraft. [4] ... Bend-Chrysler 820 engines of 8 hp at ...
The aircraft has a standard empty weight of 250 lb (113 kg). It features a cable-braced hang glider-style high wing, weight-shift controls, an open cockpit, tricycle landing gear and a single engine in pusher configuration. [1] The aircraft is made from bolted-together aluminum tubing, with its single-surface wing covered in Dacron sailcloth.
The aircraft can be disassembled by one person in 45 minutes for ground transportation on a car top or for storage. The factory standard powerplant supplied with the Mite-Lite was the 28 hp (21 kW) Rotax 277 single cylinder, two-stroke aircraft engine. [1] Production of all models ended when the company went out of business in 1998. [1]
He modified the prototype Kitfox Lite to meet FAR 103 regulations requiring an ultralight aircraft to have an empty weight of less than 254 lb (115 kg). [1] [2] [3] [5] The fuselage is made from 4130 steel tubing. Flaperons and vortex generators are used to improve roll control and low speed flight. The wings are foldable for storage. [1] [2] [3]
The Rotax 503 is a 37 kW (50 hp), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft. [1] [2] For decades the engine was one of the most popular and reputedly reliable aircraft engines in its class (two-stroke, under 60 horsepower), [3] and it remains widely used and ...
The powerplant is a twin cylinder, air-cooled, two-stroke, single-ignition 40 hp (30 kW) Rotax 447 engine or the twin-cylinder, in-line, two-stroke 32 hp (24 kW) Kawasaki 340. With the Kawasaki 340 engine the aircraft has an empty weight of 205 lb (93 kg) and a gross weight of 400 lb (181 kg), giving a useful load of 195 lb (88 kg).
The aircraft's single surface wing is made from bolted-together aluminum tubing and covered in Dacron sailcloth. The 11.15 m (36.6 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine ...
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category and the US light-sport aircraft rules. [2] [3] It features a strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, retractable wheeled tricycle landing gear and dual floats and a single engine in pusher configuration.
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