Flat-four piston aircraft engine family by Lycoming
For a similarly named and broadly similar aircraft engine by another manufacturer, see
Continental IO-360 .
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 horsepower.[ 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 hours[ 1] or twelve years.[ 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 .[ 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.[ 4] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by 3 ⁄16 inch (4.76 mm), developing 210 hp (157 kW).[ 5] [ 6]
The O-360 family of engines comprises 167 different models with 12 different prefixes. All have a 361-cubic-inch (5.92-liter) displacement and 5.125 and 4.375 in (130.2 and 111.1 mm) bore and stroke .[ 4] [ 7] [ 8] [ 9]
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[ 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
Piper PA-44-180 Seminole features two Lycoming O-360 engines
O-360
LO-360
IO-360
LIO-360
An LIO-360 on the starboard wing of a Piper PA-34-200 Seneca I .
AIO-360
AEIO-360
HIO-360
LHIO-360
Specifications (O-360-A1A)[ edit ]
Data from Type Certificate Data Sheet E-286[ 4]
General characteristics
Components
Fuel type: 91/96 avgas minimum grade[ 15]
Oil system: 8 US qt (8 L) wet sump
Cooling system: air-cooled
Power output: 180 hp (134 kW) at 2700 rpm
Compression ratio : 8.5:1
Fuel consumption: 7.8 US gal (30 L) to 9 US gal (34 L) per hour[ 16]
Related lists
^ a b Lycoming (2004). "360 Series" (PDF) . Archived from the original (PDF) on November 26, 2010. Retrieved September 16, 2008 .
^ Lycoming Engines (July 8, 2013). "Recommended Time Between Overhaul Periods" (PDF) . Archived from the original (PDF) on September 13, 2013. Retrieved July 8, 2013 .
^ Enfield, Samuel; Burr, R.; Badgett, R.; et al., eds. (April 15, 1966). Airboats (PDF) (Technical report). San Francisco: Army Concept Team in Vietnam. p. 2. R-1590 0. Archived from the original (PDF) on August 3, 2020 – via DTIC .
^ a b c Federal Aviation Administration (August 2009). "Type Certificate Data Sheet No. E-286 Revision 20" (PDF) . Retrieved September 9, 2011 .
^ Lycoming Engines (n.d.). "Lycoming IO-390-X" . Retrieved January 7, 2009 .{{cite web }}
: CS1 maint: year (link )
^ Lycoming Engines (2004). "Specialty datasheet" (PDF) . Retrieved December 20, 2008 .
^ Federal Aviation Administration (January 10, 2018). "Type Certificate Data Sheet No. 1E10 Revision 28" (PDF) . Retrieved January 26, 2019 .
^ Federal Aviation Administration (March 1986). "Type Certificate Data Sheet No. E26EA Revision 4" . Retrieved January 18, 2009 .
^ Federal Aviation Administration (March 1986). "Type Certificate Data Sheet No. E16EA Revision 5" . Retrieved January 18, 2009 .
^ Federal Aviation Administration (July 13, 2004). "Airplane Flying Handbook" (PDF) . Archived from the original (PDF) on September 21, 2012. Retrieved September 18, 2012 .
^ Mooney Aircraft, Inc. (March 1967). Executive 21 Owners Manual .
^ https://hartzellprop.com/SERVICE-DOCUMENTS/SB/HC-SB-61-227.pdf
^ Hartzell Propeller Inc. (August 27, 2012). SERVICE BULLETIN HC-SB-61-227 (Rev 6) Page 19 .
^ a b Federal 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 .
^ Lycoming (2010). "Lycoming Service Instruction 1070Q" (PDF) . Archived from the original (PDF) on November 17, 2011. Retrieved November 3, 2011 .
^ "O-360, HO-360, IO-360, AIO-360, HIO-360 & TIO-360 Operator's Manual" . lycoming.com . Retrieved July 11, 2018 .