250-C10D is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Control system: Hydromechanical
Dry weight: 63 kilogram
Gas generator stages: 2
Max. continuous power: 201 kilowatt
Max. takeoff power: 236 kilowatt
Ng RPM: 51120
Output shaft RPM: 6000
Power turbine stages: 2
ICAO: B06
View Type →ICAO: B06
View Type →