TYPE: Advanced jet trainer/light attack jet

PROGRAMME: Revealed as feasibility study at Aviation Expo 2001, Beijing, September 2001.

DESIGN FEATURES: Shoulder-mounted wings with curved, leading-edge wingroot strakes; tandem cockpits; twin engines; single vertical fin well forward of slab tailplane.

FLYING CONTROLS: Assumed fly-by-wire.

POWER PLANT: Twin turbofans; possibly NMKB Progress AI-25s or domestic WS11s.

ACCOMMODATION: Two zero/zero ejection seats in tandem.

AVIONICS: HOTAS controls, HUD(s) and MFDs; stores management system.

DIMENSIONS, EXTERNAL:  
Wing span 11 m (36 ft)
Length overall 15 m (49 ft)
WEIGHTS AND LOADINGS:  
Normal T-O weight, clean 6,500 kg (14,330 lb)
Max T-O weight 9,500 kg (20,950 lb)
PERFORMANCE:  
Max level speed M1.4
Max rate of climb at S/L 9,000 m (29,530 ft)/min
Service ceiling 16,000 m (52,490 ft)
g limits +8/-3