250-C30M is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 1
Control system: Hydromechanical
Dry weight: 114 kilogram
Gas generator stages: 2
Height: 0.65 metre
Length: 1.1 metre
Max. continuous power: 447 kilowatt
Max. continuous torque: 71 decanewton-metre
Max. takeoff power: 485 kilowatt
Max. takeoff torque: 80 decanewton-metre
Max. transient overtorque: 86.4 decanewton-metre
Ng RPM: 51000
Output shaft RPM: 6016
Power turbine stages: 2
Width: 0.56 metre
