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Light Wing AC4 : ウィキペディア英語版 | Light Wing AC4
The Light Wing AC4 is a Swiss ultralight and light-sport aircraft, designed by Hans Gygax and produced by Light Wing AG Aviation of Stans. 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 63. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The AC4 was designed to comply with the Fédération Aéronautique Internationale microlight rules and US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.〔 The aircraft is made from a combination of composites and aluminum sheet, with its tailboom made from a single large diameter aluminium tube and the wings and tail surfaces covered in aluminium. Its span wing has an area of , is supported by V-struts and mounts flaps. The standard engine available is the Rotax 912ULS four-stroke powerplant.〔 The AC4 can optionally be fitted with two extra seats in the luggage compartment and was also designed for aero-towing gliders. It can also accommodate a stretcher for Medevac missions.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Light Wing AC4」の詳細全文を読む
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