PT6C-67D is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 5
Gas generator stages: 1
Max. continuous power: 882 kilowatt
Max. continuous torque: 39.6 decanewton-metre
Max. takeoff power: 882 kilowatt
Max. takeoff torque: 39.6 decanewton-metre
Max. transient overtorque: 54.2 decanewton-metre
Power turbine stages: 2
