Initial Operational Capability (IOC):
Total Production: ?
Also Known As: O-360-J2A
Origin: United States of America
Corporations: Lycoming
Parent System: O-360
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Lycoming O-360 is a 4-cylinder helicopter engine developing up to 145 horsepower of power output. The O-360 engine is powering the Robinson R22 helicopter.

O-360 Applications

Private Aircraft R22 Beta II

O-360 Specifications

Fan Pressure Ratio: 8.50
RPM: 2,400
Height: 23.0 inch (584 millimeter)
Length: 29.8 inch (757 millimeter)
Width: 32.2 inch (819 millimeter)
Max Power at TakeOff: 145 hp (108 kW)
Dry Weight: 258 pound (117 kilogram)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


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