T5307A is a turboprop engine model used in aircraft.
Engine Family: turboprop
Output shaft RPM: 1710
Compressor stages: 6
Dry weight: 254 kilogram
Gas generator stages: 1
Length: 1.44 metre
Max. continuous power: 746 kilowatt
Max. continuous torque: 444.7 decanewton-metre
Max. takeoff power: 820 kilowatt
Max. takeoff torque: 485.4 decanewton-metre
Power turbine stages: 1
