Rover L-267 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 104.78 millimetre
Compression ratio: 5.15
Cooling system: Air
Cylinder configuration: Inline
Cylinder count: 3
Displacement: 4380 cubic-centimetre
Dry weight: 105 kilogram
Fuel grade: 59
Fuel type: Avgas
Max. continuous RPM: 1975
Max. continuous hp: 75 horsepower
Max. takeoff RPM: 1975
Max. takeoff hp: 75 horsepower
Stroke: 127 millimetre
ICAO: -
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