A75-9J is a piston engine model used in aircraft.
Engine Family: piston
Bore: 98.43 millimetre
Compression ratio: 6.3
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 2802 cubic-centimetre
Dry weight: 78 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2600
Max. continuous hp: 75 horsepower
Max. takeoff RPM: 2600
Max. takeoff hp: 75 horsepower
Stroke: 92.08 millimetre
ICAO: L8
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