Friday, August 29, 2008

O-360

Also Known As: O-360-J2A

Origin:United States of America

Contractor/s: Lycoming

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.

Specifications
Dimensions: Height 22.99 in, Length 29.81 in, Width 32.24 in

Weights: Dry Weight 258 lb (117 kg)

Power: Power 145 hp

Other: Fan Pressure Ratio 9, RPM 2,400

Applications
R22 Beta II Operators

United States of America

Internet Resources
lycoming.textron.com, lycoming.textron.com

Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)

Last Updated: Sunday, August 24, 2008

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