Genet Major I is a piston engine model used in aircraft.
Engine Family: piston
Bore: 107.95 millimetre
Compression ratio: 5.35
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 5
Displacement: 5231 cubic-centimetre
Dry weight: 110 kilogram
Fuel grade: 77
Fuel type: Avgas
Max. continuous RPM: 2200
Max. continuous hp: 106 horsepower
Max. takeoff RPM: 2200
Max. takeoff hp: 105 horsepower
Stroke: 114.3 millimetre
