FC-31

FC-31  CHARACTERISTICS

General characteristics

Crew: one (pilot)
Length: 17.3 m (56 ft 9 in)
Wingspan: 11.5 m (37 ft 9 in)
Height: 4.8 m (15 ft 9 in)
Wing area: 50 m2 (540 sq ft) [67]
Max takeoff weight: 28,000 kg (61,729 lb) 
Powerplant: 2 × WS-13 afterburning turbofans, 87.2 kN (19,600 lbf) thrust each
Powerplant: 2 × WS-19[54] afterburning turbofans, 110 kN (24,000 lbf) thrust each
Performance

Maximum speed: Mach 1.8 at high altitude
Mach 1.14 (1,400 km/h, 870 mph) at sea level
Combat range: 1,200 km (750 mi, 650 nmi) on internal fuel, or 1,900 kilometres (1,200 mi) with aerial refueling
Service ceiling: 16,000 m (52,000 ft)
Armament
Hardpoints: 6 x external, and internal bay[69] with a capacity of up to 8,000 kilograms (18,000 lb),[70] including 2,000 kilograms (4,400 lb) internally[69]
Missiles:
Air-to-air missiles:
12 x medium-range
Air-to-ground missiles:
8 x supersonic
Bombs:
8 × 500 kg deep-penetration bombs
30 x smaller bombs
Avionics
KLJ-7A[68] AESA radar
Distributed aperture system (DAS) optical early-warning system
Electro-optical targeting system (EOTS)