PT6A-25C is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 4
Control system: Hydromechanical
Dry weight: 161 kilogram
Gas generator stages: 1
Height: 0.58 metre
Length: 1.6 metre
Max. continuous power: 559 kilowatt
Max. takeoff power: 559 kilowatt
Ng RPM: 37468
Output shaft RPM: 2200
Power turbine stages: 1
Width: 0.58 metre
