250-C28C is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 1
Control system: Hydromechanical
Dry weight: 107 kilogram
Gas generator stages: 2
Height: 0.65 metre
Length: 1.1 metre
Max. continuous power: 373 kilowatt
Max. continuous torque: 62.8 decanewton-metre
Max. takeoff power: 373 kilowatt
Max. takeoff torque: 62.8 decanewton-metre
Max. transient overtorque: 83 decanewton-metre
Ng RPM: 50940
Output shaft RPM: 6016
Power turbine stages: 2
Width: 0.56 metre
ICAO: B105
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