Leopard IIIA is a piston engine model used in aircraft.
Engine Family: piston
Bore: 152.4 millimetre
Compression ratio: 5.1
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 14
Displacement: 48650 cubic-centimetre
Dry weight: 733 kilogram
Fuel type: Avgas
Max. continuous RPM: 1700
Max. continuous hp: 800 horsepower
Max. takeoff RPM: 1700
Max. takeoff hp: 800 horsepower
Stroke: 190.5 millimetre
