Cirrus Minor I is a piston engine model used in aircraft.
Engine Family: piston
Bore: 100.08 millimetre
Compression ratio: 5.8
Cooling system: Air
Cylinder configuration: Inline
Cylinder count: 4
Displacement: 3996 cubic-centimetre
Dry weight: 91 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 2300
Max. continuous hp: 82 horsepower
Max. takeoff RPM: 2300
Max. takeoff hp: 82 horsepower
Stroke: 127 millimetre
ICAO: -
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