Initial Operational Capability (IOC):
Total Production: ?
Also Known As: AEIO-540-D4D5 and IO-540
Origin: United States of America
Corporations: Lycoming
Parent System: O-540
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Lycoming O-540 is a six-cylinder helicopter engine developing up to 235-hp of power. The IO-540 engines are equipped with fuel injection system. The IO-540 engine powers the Robinson R44 helicopter.

O-540 Applications

Combat Aircraft Grob 120A Private Aircraft R44 Raven II

O-540 Specifications

Fan Pressure Ratio: 8.50
RPM: 2,800
Height: 24.6 inch (624 millimeter)
Length: 37.2 inch (945 millimeter)
Width: 33.4 inch (848 millimeter)
Max Power at TakeOff: 235 hp (175 kW)
Dry Weight: 369 pound (167 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)

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