Engine structure :
Twin-shaft, bypass turbofan engine
3-stage LP compressor with intel guide vane
6-stage HP compressor (3 stages with variable stator vanes)
Annular combustion chamber
Single-stage cooled HP turbine
Single-stage cooled LP turbine
Radial A/B chamber
Variable-section convergent flap-type nozzle
Full authority digital engine control(FADEC)
Modular on-condition maintenance(21modules)