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InterPlane Griffon : ウィキペディア英語版 | InterPlane Griffon
The InterPlane Griffon is a single seat, high wing, single engine, pusher configuration, tricycle gear ultralight aircraft, that was produced in kit form from InterPlane Aircraft of Zbraslavice, Czech Republic.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 181. BAI Communications. ISBN 0-9636409-4-1〕〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page B-27 Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕 ==Development== The Griffon was the first design produced by InterPlane when they opened for business in 1992. The Griffon was designed for the requirements of the US FAR 103 ''Ultralight Vehicles'' category, including that category's maximum empty weight.〔〔〔 The Griffon airframe is constructed from aluminum tubing, with the wings and tail covered with doped aircraft fabric. The wing is supported by a "V" strut and utilizes jury struts. It features a three tube tail that allows the pusher propeller to be located in between the tail booms. Standard features supplied included brakes, electric starting, wheel pants, elevator trim system and a plastic cockpit pod fairing with a windshield. The wings and tail surfaces can be folded for trailering or storage.〔〔 Available engines included the Rotax 447 and the Rotax 503.〔〔
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「InterPlane Griffon」の詳細全文を読む
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