PT6A-25 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 4
Control system: Hydromechanical
Dry weight: 164 kilogram
Gas generator stages: 1
Height: 0.58 metre
Length: 1.6 metre
Max. continuous power: 410 kilowatt
Max. takeoff power: 410 kilowatt
Ng RPM: 37468
Output shaft RPM: 2200
Power turbine stages: 1
Width: 0.58 metre
ICAO: T34T
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