B-54 is a piston engine model used in aircraft.
Engine Family: piston
Bore: 117.48 millimetre
Compression ratio: 5.25
Cooling system: Air
Cylinder configuration: Radial
Cylinder count: 5
Displacement: 7227 cubic-centimetre
Dry weight: 200 kilogram
Fuel grade: 73
Fuel type: Avgas
Max. continuous RPM: 1925
Max. continuous hp: 125 horsepower
Max. takeoff RPM: 1925
Max. takeoff hp: 125 horsepower
Stroke: 133.35 millimetre