Lycoming O-360
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O-360 | |
---|---|
Lycoming IO-360-A1B6 | |
Type | Piston aero-engine |
Manufacturer | Lycoming Engines |
First run | c.1955 |
Major applications | Piper Cherokee Cessna 172 Robin DR400 |
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.[1]
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[1] or twelve years.[2]
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.[3] The Lycoming IO-390 is an O-360 which has had its cylinder bore increased by Lua error in Module:Convert at line 452: attempt to index field 'titles' (a nil value)., developing 210 hp (157 kW) .[4][5]
Contents
Series
The O-360 family of engines comprise 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.[3][3][6][6][7][8]
- 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[9]
- 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
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Applications
- O-360
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- LO-360
- IO-360
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- Adventure Air Adventurer
- AeroCad AeroCanard
- Aircraft Technologies Acro 1
- Australian Lightwing SP-6000
- Aviat Husky A-1C-200
- Beechcraft Musketeer Super III
- Brutsche Freedom 210 STOL
- CEI Free Spirit Mk II
- Cessna 172R/172S
- Cessna 177RG
- Cessna 336 Skymaster
- Commander 112
- Commander 114
- Diamond DA40
- Diamond DA42
- Dream Tundra
- Evektor VUT100-120i Cobra
- Falconar SAL Mustang
- Giles G-200
- Glassic SQ2000
- Lake LA-4-200 Buccaneer
- LFU 205
- Mooney M20[10]
- Mustang Aeronautics Mustang II
- Osprey GP4
- PAC CT/4
- Partenavia P.68
- Peña Bilouis
- Peña Dahu
- Piper Arrow
- Piper PA-34 Seneca I
- Sawyer Skyjacker II
- Scaled Composites Boomerang
- Skipper Scrappy UAC-200
- Scottish Aviation Bulldog
- Seawind 2000
- SGP M-222 Flamingo
- Socata Tobago TB200XL
- Sorrell Hiperbipe
- Stolp Super Starduster
- Tecnam P2010
- Thorp T-18
- Ultimate 10-200
- Van's Aircraft RV-6
- Van's Aircraft RV-7
- Van's Aircraft RV-8
- Zeppelin NT
- Zlín Z 42
- LIO-360
- AIO-360
- AEIO-360
- Aero-Cam Slick 360
- Aviat Eagle II
- Bellanca Super Decathlon
- Extra EA-200
- FFA AS-202 Bravo
- Grob G 115E
- Mudry CAP 10
- Peña Capeña
- Pitts Special
- Tech Aero TR 200
- Valmet L-70 Vinka
- HIO-360
- LHIO-360
Specifications (O-360-A1A)
Data from Type Certificate Data Sheet E-286[3]
General characteristics
- Type: Four-cylinder, dual magneto, horizontally opposed, four-stroke aircraft engine
- Bore: 5.125 in (130 mm)
- Stroke: 4.375 in (111 mm)
- Displacement: 361 cu in (5,916 cc)
- Dry weight: 258 lb (117 kg)
Components
- Fuel type: 91/96 avgas minimum grade[12]
- Oil system: 8 US qt (8 L) dry sump
- Cooling system: air-cooled
Performance
- Power output: 180 hp (134 kW) at 2700 rpm
- Compression ratio: 8.5:1
See also
References
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External links
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