225-C10A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Control system: Hydromechanical
Dry weight: 73 kilogram
Gas generator stages: 2
Max. continuous power: 261 kilowatt
Max. takeoff power: 261 kilowatt
Ng RPM: 50970
Output shaft RPM: 6016
Power turbine stages: 2
