Cheetah IX is a piston engine model used in aircraft.
Engine Family: piston
Bore: 133.35 millimetre
Compression ratio: 6.35
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 7
Displacement: 13658 cubic-centimetre
Dry weight: 288 kilogram
Fuel grade: 87
Fuel type: Avgas
Max. continuous RPM: 2100
Max. continuous hp: 310 horsepower
Max. takeoff RPM: 2100
Max. takeoff hp: 340 horsepower
Stroke: 139.7 millimetre
