T5311A is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 6
Dry weight: 225 kilogram
Gas generator stages: 1
Length: 1.21 metre
Max. continuous power: 671 kilowatt
Max. continuous torque: 115.2 decanewton-metre
Max. takeoff power: 820 kilowatt
Max. takeoff torque: 125.5 decanewton-metre
Output shaft RPM: 6610
Power turbine stages: 1
