PT6A-45 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 4
Control system: Hydromechanical
Dry weight: 202 kilogram
Gas generator stages: 1
Height: 0.46 metre
Length: 1.85 metre
Max. continuous power: 760 kilowatt
Max. takeoff power: 875 kilowatt
Ng RPM: 37468
Np RPM: 29894
Output shaft RPM: 1700
Power turbine stages: 2
Width: 0.46 metre
ICAO: SS2T
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