H-63P is a piston engine model used in aircraft.
Engine Family: piston
Bore: 68.26 millimetre
Compression ratio: 8.1
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 1032 cubic-centimetre
Dry weight: 30 kilogram
Fuel grade: 80/87
Fuel type: Avgas
Max. continuous RPM: 4000
Max. continuous hp: 45 horsepower
Max. takeoff RPM: 4400
Max. takeoff hp: 48 horsepower
Stroke: 69.85 millimetre
