| Specifications |
|---|
| Builder | Nanchang/Hongdu
|
| Technical Data |
|
| Dimensions |
|
| Overall length | 11.6 m
|
| Overall height | 4.21 m
|
| Wing area | 17.02 m2
|
| Wing span | 9.63 m
|
| Wheel track | 2.54 m
|
| Wheel base | 4.442 m
|
| Weights |
|
| Normal take-off weight | 3700 kg
|
| Useful load | 943 kg
|
| Internal fuel capacity | 780 kg
|
| Weight empty | 2757 kg
|
| Max take-off weight | 4332 kg
|
| Engine | WS-11 turbofan (Chinese copy of Ukrainian AI-25TLK)
|
| Rated power Max static thrust at sea level | 3600 lbs
|
| SFC | 0.502 lb/lb thrust hr (Max static thrust)
|
| Air flow | 115 lbs /sec (take-off and max continuous)
|
| Engine net weight | 812 lb
|
| Pressure ratio | 13.9
|
| Bypass ratio | 2.67
|
| An access through which the engine is installed/removed is provided on the belly of the fuselage. With this provision, replacement of the engine in the field takes £ 50 minutes.
|
| Flight Performance |
|
| Max speed | Mach 0.75 / 513 kts / 950 kmh / 590 mph
|
| Max level speed | 800 km/hr
|
| Rate of climb at sea level | 30 m/s
|
| Service ceiling | 13600 m
|
| Built-in Range | 1560 km
|
| Ferry range (with drop tanks) | 2140 km
|
| Endurance | 3.2 hrs
|
| Max endurance (with drop tanks) | 4.2 hrs
|
| Unstick speed | 185 km/hr
|
| Touchdown speed | 160 km/hr
|
| Take-off ground run | 440 m
|
| Landing ground run | 530 m
|
| Limit load factor | +7.33 g -3.0 g
|
| Armament |
Option for 23 mm belly-mounted cannon
4 underwing hardpoints capable of 943 kg (2,078 lbs.) of ordnance, including PL-7 anti-aircraft missiles, bombs, or rockets
|
| Crew |
|
| Cost |
|
