A-65-7 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: 74 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2350
Max. continuous hp: 65 horsepower
Max. takeoff RPM: 2350
Max. takeoff hp: 65 horsepower
Stroke: 92.08 millimetre
ICAO: ERCO
View Type →ICAO: AR65
View Type →ICAO: AR6T
View Type →ICAO: L8
View Type →ICAO: TAYB
View Type →ICAO: TAYD
View Type →ICAO: J3
View Type →ICAO: J4
View Type →ICAO: J3
View Type →ICAO: J3
View Type →ICAO: TAYD
View Type →ICAO: AR6T
View Type →