C-125-2 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 103.17 millimetre
Compression ratio: 6.3
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 6
Displacement: 4621 cubic-centimetre
Dry weight: 114 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2550
Max. continuous hp: 125 horsepower
Max. takeoff RPM: 2550
Max. takeoff hp: 125 horsepower
Stroke: 92.08 millimetre
ICAO: CLA
View Type →ICAO: GC1
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