A-10 Thunderbolt II Specifications

Primary Function: A-10 -- close air support, OA-10 - airborne forward air control

Contractor: Fairchild Republic Co. (FRC acquired in 1987, now part of Northrop Grumman ISER)

Power Plant: Two General Electric TF34-GE-1 00 turbofans

Thrust: 9,065 pounds each engine

Wingspan: 57 feet, 6 inches (17.42 meters)

Length: 53 feet, 4 inches (16.16 meters)

Height: 14 feet, 8 inches (4.42 meters)

Weight: 29,000 pounds (13,154 kilograms)

Maximum Takeoff Weight: 51,000 pounds (22,950 kilograms)

Fuel Capacity: 11,000 pounds (7,257 kilograms)

Payload: 16,000 pounds (7,257 kilograms)

Speed: 420 miles per hour (Mach 0.56)

Range: 800 miles (695 nautical miles)

Ceiling: 45,000 feet (13,636 meters)

Armament: One 30 mm GAU-8/A seven-barrel Gatling gun; up to 16,000 pounds (7,200 kilograms) of mixed ordnance on eight under-wing and three under-fuselage pylon stations, including 500 pound (225 kilograms) Mk-82 and 2,000 pounds (900 kilograms) 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; jammer pods; 2.75-inch (6.99 centimeters) rockets; illumination flares and AIM-9 Sidewinder missiles.

Crew: One

Initial operating capability: A-10A, 1977; A-10C, 2007

Inventory: Active force, A-10, 143 and OA-10, 70; Reserve, A-10, 46 and OA-10, 6; ANG, A-10, 84 and OA-10, 18