Entry Into service
2007-03-12
Maximum Take-Off Weight
13.5 t (paragliders: kg)
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
|
CAC/PAC JF-17 Thunder |
13.5 |
3000 |
Similar airplanes
All data (26 fields)
- Name
- CAC/PAC JF-17 Thunder
- Manufacturer
- Chengdu Aircraft Corporation
- Description
- The CAC/PAC JF-17 Thunder, also known as FC-1 Xiaolong, is a Sino-Pakistani single-engine lightweight supersonic multirole combat aircraft developed jointly by the Pakistan Aeronautical Complex (PAC) and the Chengdu Aircraft Corporation (CAC) of China.
- First Flight
- 2003-08-25
- Entry Into service
- 2007-03-12
- Designer
- Chengdu Aircraft Corporation
- Type
- Multirole Combat Aircraft
- Length (m)
- 14.33
- Height (m)
- 4.57
- Cockpit Crew
- 1
- Max Speed (km/h)
- 1910
- Min Speed (km/h)
- 150
- Max Ceiling (m)
- 16916
- Rate of Climb (m/s)
- 300
- Armament
- 1 × 23 mm GSh-23 twin-barrel cannon; ; Unguided bombs:; 250 kg — Pre-fragmented Bomb; Pk-82 — (General-Purpose Bomb); Pk-83 — (General-Purpose Bomb); PK-84 — (General-Purpose Bomb); HAFR-1 — (Anti-runway Bomb); HAFR-2 — (Anti-runway Bomb); RPB-1 — (Anti-runway Bomb); BLU-107 — (Anti-runway Bomb); Mk 20 Rockeye II — (Cluster Bomb); Guided bombs:; H-2 SOW — (Glide Bomb); H-4 SOW — (Glide Bomb); GBU…
- Max Mach (Mach)
- 1.8
- National Origin
- Pakistan
- Number Built
- 200
- Powerplant Description
- 1 × Klimov RD-93MA afterburning turbofan (91.2 kN (20,500 lbf) thrust with afterburner) with Full Authority Digital Engine Control (FADEC) (previous engine: 1 x Klimov RD-93 afterburning turbofan (84.4 kN (18,974 lbf) thrust with afterburner)
- Primary Users
- Pakistan Air Force, Myanmar Air Force, Nigerian Air Force, Azerbaijani Air Forces
- Status
- In service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/CAC/PAC_JF-17_Thunder
- Flat Wing Span (m)
- 9.44
- Flat Wing Area (m²)
- 24.43
- Aircraft Engine
- Klimov RD-33
- Number of Engines
- 1