M 137 A is a piston engine model used in aircraft.
Engine Family: piston
Bore: 105 millimetre
Compression ratio: 6.3
Cooling system: Air
Cylinder configuration: Inline
Cylinder count: 6
Displacement: 5970 cubic-centimetre
Dry weight: 147 kilogram
Max. continuous RPM: 2680
Max. continuous hp: 158 horsepower
Max. takeoff RPM: 2750
Max. takeoff hp: 178 horsepower
Stroke: 115 millimetre
ICAO: Z26
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