250-C300/A1 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Control system: Hydromechanical
Dry weight: 91 kilogram
Gas generator stages: 2
Height: 0.6 metre
Length: 0.95 metre
Max. continuous power: 179 kilowatt
Max. continuous torque: 33.1 decanewton-metre
Max. takeoff power: 224 kilowatt
Max. takeoff torque: 39 decanewton-metre
Max. transient overtorque: 58.3 decanewton-metre
Ng RPM: 50970
Output shaft RPM: 6016
Power turbine stages: 2
Width: 0.55 metre
ICAO: R66
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