PT6A-67AF is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 5
Control system: Hydromechanical
Dry weight: 241 kilogram
Gas generator stages: 1
Height: 0.47 metre
Length: 1.92 metre
Max. continuous power: 910 kilowatt
Max. continuous torque: 518.6 decanewton-metre
Max. takeoff power: 1062 kilowatt
Max. takeoff torque: 596.6 decanewton-metre
Max. transient overtorque: 691.5 decanewton-metre
Ng RPM: 37468
Np RPM: 29894
Output shaft RPM: 1700
Power turbine stages: 2
Width: 0.47 metre
ICAO: AT8T
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