CTS800-4A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 2
Control system: Dual FADEC
Dry weight: 170 kilogram
Gas generator stages: 2
Max. continuous power: 963 kilowatt
Max. continuous torque: 38.1 decanewton-metre
Max. takeoff power: 1024 kilowatt
Max. takeoff torque: 41.1 decanewton-metre
Ng RPM: 43796
Np RPM: 23000
Power turbine stages: 2
