F10 A1A is a piston engine model used in aircraft.
Engine Family: piston
Bore: 58 millimetre
Compression ratio: 8.7
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 570 cubic-centimetre
Dry weight: 25 kilogram
Fuel grade: RON 91
Fuel type: Mogas
Max. continuous RPM: 5000
Max. continuous hp: 26 horsepower
Max. takeoff RPM: 5000
Max. takeoff hp: 26 horsepower
Stroke: 54 millimetre
ICAO: -
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