M 137 C is a piston engine model used in aircraft.
Engine Family: piston
Bore: 105 millimetre
Compression ratio: 7.4
Cooling system: Air
Cylinder configuration: Inline
Cylinder count: 6
Displacement: 5970 cubic-centimetre
Dry weight: 147 kilogram
Max. continuous RPM: 2700
Max. continuous hp: 185 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 202 horsepower
Stroke: 115 millimetre
