TM 333 2B2 is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 3
Control system: Single channel EECU
Dry weight: 167 kilogram
Gas generator stages: 1
Height: 0.75 metre
Length: 1.05 metre
Max. continuous power: 736 kilowatt
Max. continuous torque: 108.8 decanewton-metre
Max. takeoff power: 825 kilowatt
Max. takeoff torque: 123 decanewton-metre
Max. transient overtorque: 136 decanewton-metre
Ng RPM: 45000
Np RPM: 37562
Output shaft RPM: 6000
Power turbine stages: 1
Width: 0.45 metre
