Cirrus Major I is a piston engine model used in aircraft.
Engine Family: piston
Bore: 119.89 millimetre
Compression ratio: 5.1
Cooling system: Air
Cylinder configuration: Inline
Cylinder count: 4
Displacement: 6320 cubic-centimetre
Dry weight: 141 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2100
Max. continuous hp: 145 horsepower
Max. takeoff RPM: 2100
Max. takeoff hp: 145 horsepower
Stroke: 139.95 millimetre
