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The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines. Engines in the O-360 series produce between 145 and 225 horsepower (109 to 168 kW), with the basic O-360 producing 180. The engine family has been installed in thousands of aircraft, including the Cessna 172, Piper Cherokee/Archer, Grumman Tiger, and many home-built craft. It has a factory rated time between overhaul (TBO) of 2000 hours〔 or twelve years. The first O-360 certified was the A1A model, certified on 20 July 1955 to United States CAR 13 effective March 5, 1952 as amended by 13-1 and 13-2.〔 The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by , developing . ==Series== The O-360 family of engines comprise 167 different models with 12 different prefixes. All have a displacement and bore and stroke.〔〔 * O-360 carbureted series * HO-360 horizontally mounted series for helicopter installation * LO-360 same as O-360, but with left-hand rotating crankshaft, for use in pairs on twin-engined aircraft * TO-360 turbocharged series * LTO-360 turbocharged left-hand rotation series * IO-360 fuel-injected series * LIO-360 same as IO-360, but with left-hand rotating crankshaft * AIO-360 inverted mount (dry sump aerobatic) fuel-injected series * AEIO-360 aerobatic fuel-injected series * HIO-360 horizontally mounted fuel-injected series for helicopters * LHIO-360 left-hand rotation, fuel-injected, horizontally mounted for helicopters * TIO-360 turbocharged and fuel-injected series 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-360」の詳細全文を読む スポンサード リンク
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