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Convair 106 Skycoach : ウィキペディア英語版 | Convair 106 Skycoach
The Convair Model 106 Skycoach was an experimental four-seat light aircraft, designed and built by the Stinson Division of Convair at the end of the Second World War.〔 ==Design and development== The Model 106 was a four-seat cabin aircraft with a pusher engine, fixed spatted tricycle undercarriage and twin tail booms flanking the propeller. The three passengers and pilot sat in a cabin in the fuselage nacelle, which also housed the pusher Franklin 6A8-225-B8 six-cylinder horizontally-opposed piston engine, driving a cooling fan and pusher propeller.〔 Flight testing was carried out at San Diego, but performance was found to be unexceptional, comparing very poorly to the contemporary Beechcraft Bonanza, which could cruise at on only . With a maximum speed of only the Model 106 was hopelessly outclassed and Convair abandoned development, scrapping the sole prototype, (regn. NX40004, msn. 1), in 1947.〔
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「Convair 106 Skycoach」の詳細全文を読む
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