250-C47B/8 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 1
Control system: Single channel EECU + Hydromechanical backup control
Dry weight: 126 kilogram
Gas generator stages: 2
Height: 0.64 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: 6317
Power turbine stages: 2
Width: 0.56 metre
ICAO: B407
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