250-C10 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Control system: Hydromechanical
Dry weight: 62 kilogram
Gas generator stages: 2
Max. continuous power: 158 kilowatt
Max. takeoff power: 186 kilowatt
Ng RPM: 51120
Output shaft RPM: 6000
Power turbine stages: 2
ICAO: H500
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