R-266 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 107.95 millimetre
Compression ratio: 5.5
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 5
Displacement: 4359 cubic-centimetre
Dry weight: 97 kilogram
Fuel grade: 59
Fuel type: Avgas
Max. continuous RPM: 2375
Max. continuous hp: 90 horsepower
Max. takeoff RPM: 2375
Max. takeoff hp: 90 horsepower
Stroke: 95.25 millimetre
