Fairchild A-10A Thunderbolt II Aircraft Data
The A-10 Thunderbolt II is an American single-seat, twin-engine, straight-wing jet aircraft developed by Fairchild-Republic for the United States Air Force to provide close air support (CAS) of ground forces by attacking tanks, armored vehicles and other ground targets with a limited air interdiction capability. It is the first U.S. Air Force aircraft designed exclusively for close air support.
- Country of Origin: United States
- First Flight: 10 May 1972
- Initial Service Date: March 1977
- No. Built: 715
- No. In Service: 353 (approx.)
- No. of Hardpoints: 11
- Crew: 1
Power:
2x General Electric TF34-GE-100A Turbofans at 80.64 kN
Weapons:
1x 30mm GAU-8/A Avenger (1174 rounds)
4× LAU-61/LAU-68 rocket pods (19 Hydra 70mm rockets each)
4× LAU-5003 rocket pods (19 CVR7 70mm rockets each)
6× LAU-10 rocket pods (4x 127mm Zuni rockets each)
2x AIM-9 Sidewinders
8x AGM-65 Maverick
Mk 82/83/84 unguided bombs, Mk. 77 incendiary bombs, BLU-1, BLU-27/B Rockeye II, Mk. 20, BL-755, CBU-52/58/71/87/89/97 cluster bombs.
Paveway series of laser guided bombs.
4× LAU-61/LAU-68 rocket pods (19 Hydra 70mm rockets each)
4× LAU-5003 rocket pods (19 CVR7 70mm rockets each)
6× LAU-10 rocket pods (4x 127mm Zuni rockets each)
2x AIM-9 Sidewinders
8x AGM-65 Maverick
Mk 82/83/84 unguided bombs, Mk. 77 incendiary bombs, BLU-1, BLU-27/B Rockeye II, Mk. 20, BL-755, CBU-52/58/71/87/89/97 cluster bombs.
Paveway series of laser guided bombs.
Dimensions:
| Length: | 16.26 m. |
| Wing Span: | 17.53 m. |
| Wing Area: | 47 m² |
| Height: | 4.47 m. |
| Empty Weight: | 11,321 kg. |
| Max. Weight: | 23,000 kg. |
| Max. Ordnance Load: | 7,260 kg. |
Performance:
| Max. Speed: | 706 kph |
| Cruise Speed: | 560 kph |
| Service Ceiling: | 13,700 m. |
| Normal Range: | 460 km |
| Max. Range: | 4,150 km |
Random great photos of the Fairchild A-10A Thunderbolt II:
