PT6A-68 is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 5
Control system: Single channel EECU + mechanical backup control
Dry weight: 260 kilogram
Gas generator stages: 1
Height: 0.56 metre
Length: 1.81 metre
Max. continuous power: 932 kilowatt
Max. takeoff power: 932 kilowatt
Ng RPM: 37468
Output shaft RPM: 1995
Power turbine stages: 2
Width: 0.56 metre
