6A-350-D1 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 117.48 millimetre
Compression ratio: 10.5
Cooling system: Air
Cylinder configuration: Horizontally opposed
Cylinder count: 6
Displacement: 5735 cubic-centimetre
Dry weight: 138 kilogram
Fuel grade: 80/87
Fuel type: Avgas
Max. continuous RPM: 3200
Max. continuous hp: 200 horsepower
Max. takeoff RPM: 3200
Max. takeoff hp: 200 horsepower
Stroke: 88.9 millimetre
