CTS800-4N is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Output shaft RPM: 6402
Compressor stages: 2
Control system: Dual FADEC
Dry weight: 185 kilogram
Gas generator stages: 2
Max. continuous power: 955 kilowatt
Max. continuous torque: 137.3 decanewton-metre
Max. takeoff power: 1014 kilowatt
Max. takeoff torque: 147.8 decanewton-metre
Ng RPM: 43796
Np RPM: 23000
Power turbine stages: 2
