PT6A-116 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 4
Control system: Hydromechanical
Dry weight: 158 kilogram
Gas generator stages: 1
Height: 0.46 metre
Length: 1.57 metre
Max. continuous power: 522 kilowatt
Max. takeoff power: 522 kilowatt
Ng RPM: 37468
Output shaft RPM: 1900
Power turbine stages: 1
Width: 0.46 metre
