PT6C-67A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 5
Control system: Hydromechanical
Dry weight: 207 kilogram
Gas generator stages: 1
Height: 0.64 metre
Length: 1.68 metre
Max. continuous power: 1024 kilowatt
Max. continuous torque: 31.9 decanewton-metre
Max. takeoff power: 1166 kilowatt
Max. takeoff torque: 36.3 decanewton-metre
Max. transient overtorque: 59.7 decanewton-metre
Ng RPM: 37468
Np RPM: 30032
Power turbine stages: 2
Width: 0.64 metre
