CT7-6A AF is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 6
Control system: Hydromechanical
Dry weight: 224 kilogram
Gas generator stages: 2
Height: 0.64 metre
Length: 1.22 metre
Max. continuous power: 1281 kilowatt
Max. continuous torque: 66.2 decanewton-metre
Max. takeoff power: 1491 kilowatt
Max. takeoff torque: 74.2 decanewton-metre
Max. transient overtorque: 94.9 decanewton-metre
Ng RPM: 44700
Np RPM: 20463
Output shaft RPM: 20463
Power turbine stages: 2
Width: 0.66 metre
