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For a similarly named and broadly similar aircraft engine by another manufacturer, see. O-360Lycoming IO-360-A1B6TypeCertifiedNational originManufacturerFirst run1952, 1963 injected versionMajor applicationsProduced1955–presentDeveloped intoThe Lycoming O-360 is a family of, direct-drive,. Engines in the O-360 series produce between 145 and 225 horsepower (109 to 168 kW), with the basic O-360 producing 180 horsepower.The engine family has been installed in thousands of aircraft, including the, /Archer, and many craft. It has a factory rated (TBO) of 2000 hours or twelve years.
O-360 family engines are also widely used in, most notably in the used by the during the.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 is an O-360 which has had its cylinder bore increased by 3⁄ 16 inch (4.76 mm), developing 210 hp (157 kW). Contents.Series The O-360 family of engines comprise 167 different models with 12 different prefixes. An LIO-360 on the starboard wing of a.AIO-360.AEIO-360.HIO-360.LHIO-360.Specifications (O-360-A1A) Data from Type Certificate Data Sheet E-286 General characteristics.
Type: Four-cylinder,.: 5.125 in (130 mm).: 4.375 in (111 mm).: 361 cu in (5,916 cc).: 258 lb (117 kg)Components. Fuel type: 91/96 minimum grade. Oil system: 8 US qt (8 l) wet sump. Cooling system: air-cooledPerformance. Power output: 180 hp (134 kW) at 2700 rpm.: 8.5:1.
Fuel consumption: 7.8 US gal (30 L) to 9 US gal (34 L) per hourSee also.Related lists.References. ^ Lycoming (2004). Archived from (PDF) on 2010-11-26. Retrieved 2008-09-16. (8 July 2013). Archived from (PDF) on 2013-09-13. Retrieved 8 July 2013.
Enfield, Samuel; Burr, R.; Badgett, R.; et al., eds. (April 15, 1966).
Lycoming Go-480 Manual Pdf File
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Lycoming (2010). Archived from (PDF) on 17 November 2011. Retrieved 3 November 2011. Retrieved 11 July 2018.External links Wikimedia Commons has media related to.
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