6AG4-185-B12 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 114.3 millimetre
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 6
Displacement: 5490 cubic-centimetre
Fuel type: Avgas
Stroke: 88.9 millimetre
Dry weight: 149 kilogram
Compression ratio: 7
Fuel grade: 80/87
Max. continuous hp: 185 horsepower
Max. continuous RPM: 3100
Max. takeoff hp: 185 horsepower
Max. takeoff RPM: 3100