GTD-350 II is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 8
Dry weight: 138 kilogram
Gas generator stages: 1
Height: 0.76 metre
Length: 1.39 metre
Max. continuous power: 210 kilowatt
Max. takeoff power: 290 kilowatt
Ng RPM: 45000
Np RPM: 24000
Output shaft RPM: 5904
Power turbine stages: 2
Width: 0.63 metre
