| Variant | |
| Role | |
| Country | PRC |
| Builder | XAC |
| First Flight | Aug 2020 |
| Status | development |
| Number built | |
| Operators | PLAN |
| Cost | |
| Comparable Aircraft | E-2C |
| Recognition | |
| Wingspan | meters | feet |
| Sweep | |
| Wing Aspect Ratio | |
| Fuselage Maximum Diameter | meters | feet |
| length | meters | feet |
| height | meters | feet |
| wing area | sqm | sqfeet |
| Weight empty | kg | lb |
| takeoff (clean) | kg | lb |
| takeoff (maximum) | 20-25,000 kg | lb |
| Fuel, Internal | kg | lb |
| Fuel, External | kg | lb |
| Payload | kg | lb |
| Max weapon load | kg | lb |
| Armament | |
| Power Plant | |
| Thrust, max, SLS, ISA | x kg | x lbst |
| Internal fuel (usable) | kg | lb |
| Performance (clean, ISA) | |
| Max level speed (sea level) | KTAS |
| Limit speed | KEAS / MN |
| Stall speed (landing, 20% fuel) | 90 KCAS |
| Stall speed (reference) | KCAS |
| Rate of climb (SL) | feet/min |
| Service ceiling | meters | feet |
| Range / 3 ext. tanks (10% reserve) | km | nm |
| Range, ext. tanks | km | nm |
| Range, clean | km | nm |
| Endurance, clean / ext. tanks | h min / hr |
| Max sustained Load Factor (S.L.) | g |
| Max sustained Load Factor (15,000 feet) | g |
| Max sustained Turn Rate (15,000 feet) | deg/sec |
| Takeoff ground run (S.L.) | meters | feet |
| Landing ground roll (S.L., 20% internal fuel) | meters | feet |
| Limit Load factor | + g / - g |
| Crew | 5 ? |
| Accomodations | |
