The AE3007 turbofan engine is a high bypass (5:1), two spool, axial-flow engine, flat rated at 7,580 pounds of thrust, uninstalled, sea level static to 113°F ambient temperature.
The design features include:
wide-chord single-stage direct-drive fan 14-stage axial-flow compressor with inlet guide vanes (IGVs) and five variable-geometry-stator stages full annular type combustion liner with 16 fuel nozzles and two high tension igniters two-stage HP turbine driving the HP compressor three-stage LP turbine to drive the fan dual aircraft mounted, fully-redundant FADECs accessory-drive gearbox for engine-driven accessories and air system for aircraft pressurisation, engine starting, and cross bleed starts