A-40-2 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 79.38 millimetre
Compression ratio: 5.2
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 4
Displacement: 1835 cubic-centimetre
Dry weight: 65 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2550
Max. continuous hp: 37 horsepower
Max. takeoff RPM: 2550
Max. takeoff hp: 37 horsepower
Stroke: 95.25 millimetre
ICAO: J2
View Type →ICAO: J3
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