E-113A is a piston engine model used in aircraft.
Engine Family: piston
Bore: 107.95 millimetre
Compression ratio: 5.4
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 2
Displacement: 1860 cubic-centimetre
Dry weight: 55 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2400
Max. continuous hp: 36 horsepower
Max. takeoff RPM: 2400
Max. takeoff hp: 36 horsepower
Stroke: 101.6 millimetre
