AE2100A is a turboprop engine model used in aircraft.
Engine Family: turboprop
Control system: Two single channel FADEC
Max. continuous torque: 180 decanewton-metre
Max. takeoff torque: 199.3 decanewton-metre
Max. transient overtorque: 231.8 decanewton-metre
Compressor stages: 14
Dry weight: 715 kilogram
Gas generator stages: 2
Max. continuous power: 2787 kilowatt
Max. takeoff power: 3096 kilowatt
Power turbine stages: 2
Length: 2.94 metre
Width: 0.8 metre
Height: 1.26 metre
ICAO: SB20
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