A-40-4 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: 2575
Max. continuous hp: 40 horsepower
Max. takeoff RPM: 2575
Max. takeoff hp: 40 horsepower
Stroke: 95.25 millimetre
ICAO: TAYA
View Type →ICAO: J2
View Type →ICAO: J3
View Type →ICAO: AERK
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