M 208 B1 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 115 millimetre
Compression ratio: 7
Cooling system: Air
Cylinder configuration: Horizontally-opposed
Cylinder count: 6
Displacement: 7167 cubic-centimetre
Dry weight: 214 kilogram
Max. continuous RPM: 2850
Max. continuous hp: 202 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 236 horsepower
Stroke: 115 millimetre
