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Airborne T-Lite
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Airborne T-Lite : ウィキペディア英語版
Airborne T-Lite

The Airborne T-Lite is an Australian ultralight trike, designed and produced by Airborne Windsports of Redhead, New South Wales. The aircraft is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 201. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The T-Lite was designed as both a cross country powered aircraft and self-launching motor glider for soaring. The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category as well as the US FAR 103 Ultralight Vehicles rules. It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit, tricycle landing gear and a single engine in pusher configuration.〔
The aircraft is made from bolted-together aluminum tubing, with its double surface Airborne Core wing covered in Dacron sailcloth, with the top surface finished in mylar PX cloth. The span Core wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The powerplant is a purpose-designed, single cylinder, air-cooled, four-stroke, Bailey B200 engine, with electric starting and a 3.2:1 reduction drive. The aircraft has an empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload is . The permitted pilot weight range is .〔
The T-Lite is designed to be quickly disassembled for ground transport. The fuel tank is located behind the pilot's seat and can be disconnected quickly to allow transporting it independently of the aircraft for refueling.〔




抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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