R-540-3 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 127 millimetre
Compression ratio: 5.5
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 5
Displacement: 8849 cubic-centimetre
Dry weight: 164 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 1850
Max. continuous hp: 160 horsepower
Max. takeoff RPM: 1850
Max. takeoff hp: 160 horsepower
Stroke: 139.7 millimetre
