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Six Chuter SR1 : ウィキペディア英語版 | Six Chuter SR1
The Six Chuter SR1 is an American powered parachute that was designed and produced by Six Chuter of Yakima, Washington.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page D-14. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 ==Design and development== The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of . It features a parachute-style high-wing, single-place accommodation, tricycle landing gear and a single Rotax 503 engine in pusher configuration. The Rotax 582 engine was a factory option.〔 The aircraft is built from a combination of aluminium and 4130 steel tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The aircraft was factory supplied in the form of an assembly kit that requires 40 hours to complete.〔
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「Six Chuter SR1」の詳細全文を読む
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