250-C18A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Control system: Hydromechanical
Dry weight: 64 kilogram
Gas generator stages: 2
Height: 0.57 metre
Length: 1.03 metre
Max. continuous power: 201 kilowatt
Max. continuous torque: 33.8 decanewton-metre
Max. takeoff power: 236 kilowatt
Max. takeoff torque: 39.7 decanewton-metre
Max. transient overtorque: 43.4 decanewton-metre
Ng RPM: 51120
Output shaft RPM: 6000
Power turbine stages: 2
Width: 0.48 metre
ICAO: H500
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