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Avco Lycoming O-235-A : ウィキペディア英語版 | Lycoming O-235
The Lycoming O-235 is a family of four-cylinder, air-cooled, horizontally opposed piston aircraft engines that produce , derived from the earlier O-233 engine.〔Textron Lycoming: ''Operator's Manual, Textron Lycoming Aircraft Engines, Series O-235 & O-290'', 4th Edition January 1988, Pages 2-1 & 2-4, Stock # 60297-9, Textron Lycoming.〕 Well-known designs that use versions of the O-235 included the Cessna 152, Grumman American AA-1 series, Beechcraft Model 77 Skipper, Piper Tomahawk, American Champion Citabria, Piper Clipper, and the Piper PA-22-108 Colt. ==Development== The engines are all carburetor-equipped, feature dual magneto ignition and have a displacement of 233 cubic inches (3.82 L). The first O-235 model was certified on 11 February 1942.〔 The O-235 was developed into the lighter-weight Lycoming IO-233 engine for light sport aircraft.
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「Lycoming O-235」の詳細全文を読む
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