AE2100D2A is a turboprop engine model used in aircraft.
Engine Family: turboprop
Compressor stages: 14
Control system: Two single channel FADEC
Dry weight: 805 kilogram
Gas generator stages: 2
Max. continuous power: 3458 kilowatt
Max. continuous torque: 234.8 decanewton-metre
Max. takeoff power: 3458 kilowatt
Max. takeoff torque: 234.8 decanewton-metre
Max. transient overtorque: 262.1 decanewton-metre
Power turbine stages: 2
Length: 2.97 metre
Width: 0.81 metre
Height: 1.33 metre
ICAO: C27J
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