PT6C-67C is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Max. transient overtorque: 59.7 decanewton-metre
Max. takeoff torque: 38.4 decanewton-metre
Max. continuous torque: 36.3 decanewton-metre
Np RPM: 21000
Compressor stages: 5
Control system: Single channel EECU + mechanical backup control
Dry weight: 205 kilogram
Gas generator stages: 1
Height: 0.57 metre
Length: 1.5 metre
Max. continuous power: 815 kilowatt
Max. takeoff power: 861 kilowatt
Ng RPM: 38200
Power turbine stages: 2
Width: 0.57 metre
ICAO: A139
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