Lycoming O-360
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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 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).cite-ref-lycoming360specsheet-1-0[1]
The engine family has been installed in thousands of aircraft, including the Cessna 172, Piper Cherokee/Archer, Grumman Tiger, and many home-built types. It has a factory rated time between overhaul (TBO) of 2000 hourscite-ref-lycoming360specsheet-1-1[1] or twelve years.cite-ref-twelveyears-2-0[2] O-360 family engines are also widely used in airboats, most notably in the Hurricane Aircats used by the US Army during the Vietnam War.cite-ref-sf-3-0[3]
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.cite-ref-e286-4-0[4] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by 3⁄16 inch (4.8 mm), developing 210 hp (160 kW).cite-ref-io390-5-0[5]cite-ref-specsheet-6-0[6]
Contents
• Series
• Variants
• See also
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Series
• 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 aircraftcite-ref-faa-10-0[10]
• 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
Variants
Applications
O-360
• Hurricane Aircat (airboat)
• IRI T23B
• Lucas L8
• MSW One
LO-360
IO-360
• LFU 205
• Mooney M20cite-ref-executive-21-poh-11-0[11]
• PAC CT/4
• Wega 180
LIO-360
AIO-360
AEIO-360
HIO-360
LHIO-360
• Silvercraft SH-3cite-ref-fedres23feb07-14-0[14]
• Silvercraft SH-4cite-ref-fedres23feb07-14-1[14]
Specifications (O-360-A1A)
General characteristics
• Bore: 5.125 in (130 mm)
• Stroke: 4.375 in (111 mm)
• Displacement: 361 cu in (5.9 L)
• Dry weight: 258 lb (117 kg)
Components
• Oil system: 8 US qt (8 L) wet sump
• Cooling system: air-cooled
Performance
• Power output: 180 hp (130 kW) at 2700 rpm
• Compression ratio: 8.5:1
• Fuel consumption: 7.8 US gal (30 L) to 9 US gal (34 L) per hourcite-ref-16[16]
See also
References
cite-note-lycoming360specsheet-11. ↑ citereflycoming2004Lycoming (2004). "360 Series" (PDF). Archived from the original (PDF) on November 26, 2010. Retrieved September 16, 2008.
cite-note-twelveyears-22. ↑ citereflycoming-engines2013Lycoming Engines (July 8, 2013). "Recommended Time Between Overhaul Periods" (PDF). Archived from the original (PDF) on September 13, 2013. Retrieved July 8, 2013.
cite-note-e286-44. ↑ citereffederal-aviation-administration2009Federal Aviation Administration (August 2009). "Type Certificate Data Sheet No. E-286 Revision 20" (PDF). Retrieved September 9, 2011.
cite-note-io390-55. ↑ citereflycoming-enginesn-dLycoming Engines (n.d.). "Lycoming IO-390-X". Retrieved January 7, 2009.{{cite web}}: CS1 maint: year (link)
cite-note-specsheet-66. ↑ citereflycoming-engines2004Lycoming Engines (2004). "Specialty datasheet" (PDF). Retrieved December 20, 2008.
cite-note-1e10-77. ↑ citereffederal-aviation-administration2018Federal Aviation Administration (January 10, 2018). "Type Certificate Data Sheet No. 1E10 Revision 28" (PDF). Retrieved January 26, 2019.
cite-note-e26ea-88. ↑ citereffederal-aviation-administration1986Federal Aviation Administration (March 1986). "Type Certificate Data Sheet No. E26EA Revision 4". Retrieved January 18, 2009.
cite-note-e16ea-99. ↑ citereffederal-aviation-administration1986Federal Aviation Administration (March 1986). "Type Certificate Data Sheet No. E16EA Revision 5". Retrieved January 18, 2009.
cite-note-faa-1010. ↑ citereffederal-aviation-administration2004Federal Aviation Administration (July 13, 2004). "Airplane Flying Handbook" (PDF). Archived from the original (PDF) on September 21, 2012. Retrieved September 18, 2012.
cite-note-executive-21-poh-1111. ↑ citerefmooney-aircraft-inc-1967Mooney Aircraft, Inc. (March 1967). Executive 21 Owners Manual.
cite-note-1212. ↑ https://hartzellprop.com/SERVICE-DOCUMENTS/SB/HC-SB-61-227.pdf
cite-note-hc-sb-61-227-1313. ↑ citerefhartzell-propeller-inc-2012Hartzell Propeller Inc. (August 27, 2012). SERVICE BULLETIN HC-SB-61-227 (Rev 6) Page 19.
cite-note-fedres23feb07-1414. ↑ citereffederal-aviation-administration2007Federal Aviation Administration (February 2007). "Docket No. FAA-2006-25948; Directorate Identifier 2006-NE-32-AD; Amendment 39-14951; AD 2007-04-19". Archived from the original on July 13, 2011. Retrieved March 9, 2009.
cite-note-si1070q-1515. ↑ citereflycoming2010Lycoming (2010). "Lycoming Service Instruction 1070Q" (PDF). Archived from the original (PDF) on November 17, 2011. Retrieved November 3, 2011.
cite-note-1616. ↑ "O-360, HO-360, IO-360, AIO-360, HIO-360 & TIO-360 Operator's Manual". lycoming.com. Retrieved July 11, 2018.
External links
Wikimedia Commons has media related to
Lycoming O-360
.
• Lycoming Homepage
• "Operator's Manual O-360, HO-360, IO-360, AIO-360, HIO-360 & TIO-360 Series" (PDF). Lycoming. October 2005.