LTS101-600A-2 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Max. takeoff torque: 73.3 decanewton-metre
Max. continuous torque: 70.4 decanewton-metre
Max. transient overtorque: 80.5 decanewton-metre
Max. continuous power: 440 kilowatt
Max. takeoff power: 459 kilowatt
Dry weight: 115 kilogram
Length: 0.79 metre
Width: 0.49 metre
Height: 0.6 metre
Ng RPM: 47870
Np RPM: 37000
Gas generator stages: 1
Power turbine stages: 1
Compressor stages: 2
Control system: Mechanical
ICAO: AS50
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