PT6A-140 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 4
Control system: Hydromechanical
Dry weight: 189 kilogram
Gas generator stages: 1
Height: 0.48 metre
Length: 1.55 metre
Max. continuous power: 647 kilowatt
Max. takeoff power: 647 kilowatt
Ng RPM: 37468
Output shaft RPM: 1900
Power turbine stages: 1
Width: 0.48 metre
ICAO: C208
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