BUILDER(S)
CAC, Chengdu Aircraft Industrial Corp., Chengdu, Sichuan, China
USERS/PLATFORMS
China [62]
CHARACTERISTICS
CREW
1 pilot
WEIGHTS
Empty 21,450 lb ( 9,730 kg)
Takeoff 54,344 lb (24,650 kg) max
Payload 20,944 lb ( 9,500 kg) max
DIMENSIONS
Length 54 ft 2 in (16.5 m)
Height 19 ft 8 in ( 6.0 m)
Wing span 37 ft 1 in (11.3 m)
Wing area 490 sq ft (45.5 m sq)
Canard span 17 ft 5 in ( 5.3 m)
Canard area 51 sq ft ( 4.7 m sq)
PROPULSION
Engine 1 x Saturn Lyulka AL-31F (see description)
Power 27,558 lb (12,500 kg) static thrust
Fuel
internal 9,855 lb (4,470 kg)
external 12,456 lb (5,650 kg)
PERFORMANCE
Speed 1,190-1,290 kts (1,370-1,480 mph, 2,210-2,390 kmh)
Mach 1.85-2.0 max
Ceiling 59,055 ft (18,000 m)
Range 1,000 nm (1,150 mi, 1,853 km)
Radius
hi-lo-hi 1,371 nm (1,578 mi, 2,540 km)
lo-lo-lo 707 nm ( 814 mi, 1,310 km)
WEAPONS
Cannon 1 x 23-mm cannon internal
Hardpoints 13 (11 external and 2 wingtip rails)
AAM PL-8 IR, PL-9, PL-10, R-73/AA-11 Archer,
R-77/AA-12 Adder
bombs laser-guided
missiles CSS-N-4 Sardine** anti-ship, unknown air-to-
surface
other 3 x external fuel tanks
SENSORS/ELECTRONICS
Radar KLJ-3 (Elta EL/M-2035 and Zhuk-10PD are suggested
alternatives)
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