Air Power Series>1:72 die-cast display model>A-10>HA1328
A-10A Thunderbolt II AF810977, 66th Weapons Sqn., April 2005
General Background
A-10 was the first USAF aircraft designed specifically for “Close Air Support ” (CAS) . It can be described as the outcome of the experience gained in the Vietnam War and the threats of the Soviet Union armor forces during the Cold War era. The first A-10A “Thunderbolt II” was delivered October 1975 and deployment in March 1976.
A-10's pilot is protected by titanium armor around his seat and the canopy isa large bubble canopy which provides all-round vision. The aircraft is designed with dual engines and the self-sealing fuel cells are protected by internal and external foam . Extra titanium is used to protect some flight control system parts of the aircraft. All these insure the plane and pilot's safety from enemy fires.
A-10's pilot is protected by titanium armor around his seat and the canopy isa large bubble canopy which provides all-round vision. The aircraft is designed with dual engines and the self-sealing fuel cells are protected by internal and external foam . Extra titanium is used to protect some flight control system parts of the aircraft. All these insure the plane and pilot's safety from enemy fires.
The Aircraft
The 57th Wing located at Nellis AFB is home to 19 squadrons each with a different assignment.
One of these squadrons is the 66th Weapons School that was originally activated in January
1941 as the 66th Pursuit Squadron (Interceptor). A few re-designations and de-activations the
squadron was re-activated in 2003 as 66th Weapons School. Their job was to teach
graduate-level instructors in all aspects of the A-10 so after graduation they could return to active
units to provide other personnel with advanced instruction.
Specifications :
| Crew : | One |
| Main role : | A-10 - close air support, OA-10 - airborne forward air control |
| Manufacturer : | Fairchild Republic Co. |
| Power Plants : | Two General Electric TF34-GE-100 turbofans |
| Thrust : | 9,065 pounds per engine |
| Length : | 16.16 meters |
| Height : | 4.42 meters |
| Wingspan : | 17.42 meters Speed: 420 miles per hour (Mach 0.56) |
| Ceiling : | 13,636 meters |
| Maximum Takeoff Weight : | 22,950 kg. |
| Range : | 800 miles (695 nautical miles) |
| Armament : | One 30 mm GAU-8/A seven-barrel Gatling gun (fixed) |
| Maximum 7,200 kg of mixed ordnance including : 225 kg “ Mk-82 ” and 900 kg “ Mk-84 ” series low/high drag bombs, incendiary cluster bombs, combined effects munitions, mine dispensing munitions, AGM-65 Maverick missiles and laser-guided/electro-optically guided bombs , infrared countermeasure flares , electronic countermeasure chaff , jamming pods , 6.99 cm (2.75in.) rockets , illumination flares , AIM-9 Sidewinder missiles |