250-C20S is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Control system: Hydromechanical
Dry weight: 72 kilogram
Gas generator stages: 2
Height: 0.58 metre
Length: 1.04 metre
Max. continuous power: 313 kilowatt
Max. continuous torque: 52.1 decanewton-metre
Max. takeoff power: 313 kilowatt
Max. takeoff torque: 52.1 decanewton-metre
Max. transient overtorque: 52.3 decanewton-metre
Ng RPM: 50970
Output shaft RPM: 6016
Power turbine stages: 2
Width: 0.48 metre
ICAO: C06T
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