2A-120-C1 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 117.48 millimetre
Compression ratio: 8.5
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 2
Displacement: 1917 cubic-centimetre
Dry weight: 60 kilogram
Fuel grade: 100/130
Fuel type: Avgas
Max. continuous RPM: 3200
Max. continuous hp: 60 horsepower
Max. takeoff RPM: 3200
Max. takeoff hp: 60 horsepower
Stroke: 88.9 millimetre
