2AL-112-A2 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 114.3 millimetre
Compression ratio: 8
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 2
Displacement: 1835 cubic-centimetre
Dry weight: 53 kilogram
Fuel grade: 80
Fuel type: Avgas
Max. continuous RPM: 3000
Max. continuous hp: 49 horsepower
Max. takeoff RPM: 3000
Max. takeoff hp: 49 horsepower
Stroke: 88.9 millimetre
