250-C40B is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 1
Control system: Single channel EECU + Hydromechanical backup control
Dry weight: 127 kilogram
Gas generator stages: 2
Height: 0.65 metre
Length: 1.1 metre
Max. continuous power: 457 kilowatt
Max. continuous torque: 45.8 decanewton-metre
Max. takeoff power: 533 kilowatt
Max. takeoff torque: 55.5 decanewton-metre
Max. transient overtorque: 70.6 decanewton-metre
Ng RPM: 51000
Output shaft RPM: 9598
Power turbine stages: 2
Width: 0.56 metre
ICAO: B430
View Type →