A-10 Thunderbolt II

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A-10 Thunderbolt II
Role	Close air support ground-attack aircraft
Manufacturer	Fairchild-Republic
First flight	10 May 1972
Introduction	March 1977
Status	In service
Primary user	United States Air Force
Number built	715 [1]
Unit cost	US$11.7 million (average)[2]

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.

The A-10's official name comes from the Republic P-47 Thunderbolt of World War II, a fighter that was particularly effective at close air support. The A-10 is more commonly known by its nickname "Warthog" or simply "Hog".^[3] As a secondary mission, it provides airborne forward air control, guiding other aircraft against ground targets. A-10s used primarily in this role are designated OA-10.^[4]

[edit] Development

[edit] Background

Criticism that the U.S. Air Force did not take close air support seriously prompted a few service members to seek a specialized attack aircraft.^[5] In the Vietnam War, large numbers of ground-attack aircraft were shot down by small arms, surface-to-air missiles, and low-level anti-aircraft gunfire, prompting the development of an aircraft better able to survive such weapons. In addition, the UH-1 Iroquois and AH-1 Cobra helicopters of the day, which USAF commanders had said should handle close air support, were ill-suited for use against armor, carrying only anti-personnel machine guns and unguided rockets meant for soft targets. The F-4 Phantom II was pressed into close air support, but usually in emergencies, as its high cruising speed and fuel consumption hindered its ability to loiter. The lack of a gun on most F-4 variants, coupled with the relative ineffectiveness of the standard 20 mm round on M61 Vulcan-equipped F-4Es against hard targets, made strafing runs either impossible or ineffective.

[edit] A-X

On 6 March 1967, the U.S. Air Force released a Request for Information to 21 defense contractors. Their objective was to create a design study for a low-cost attack aircraft designated A-X, or "Attack Experimental". The officer in charge of the project was Colonel Avery Kay.^[5] In 1969, the Secretary of the Air Force asked Pierre Sprey to write the detailed specifications for the proposed A-X project. However, his initial involvement was kept secret due to Sprey's earlier controversial involvement in the F-X project.^[5] Sprey's discussions with A-1 Skyraider pilots operating in Vietnam and analysis of the effectiveness of current aircraft used in the role indicated the ideal aircraft should have long loiter time, low-speed maneuverability, massive cannon firepower, and extreme survivability;^[5] an aircraft that had the best elements of the Ilyushin Il-2, Henschel Hs 129 and A-1 Skyraider. The specifications also demanded that the aircraft cost less than $3 million.^[5] In May 1970, the USAF issued a modified, and much more detailed request for proposals, as the threat of Soviet armored forces and all-weather attack operations became more serious. Now included in the requirements was that the final aircraft would be designed specifically for the GAU-8 Avenger.^[6] Six companies submitted proposals to the USAF, with Northrop and Fairchild Republic selected to build prototypes: the YA-9A and YA-10A, respectively.

The YA-10A first flew on 10 May 1972. After trials and a fly-off against the YA-9A, the Air Force selected Fairchild-Republic's YA-10A on 10 January 1973 for production. There was an additional fly-off against the Ling-Temco-Vought A-7D Corsair II, the principal Air Force attack aircraft at the time, in order to prove the need to purchase a new attack aircraft. The first production A-10 flew in October 1975, and deliveries to the Air Force commenced in March 1976 to units at Davis-Monthan Air Force Base, Arizona. The first squadron to use the A-10 went operational in October 1977. In total, 715 airplanes were produced, the last delivered in 1984.^[6]

One experimental two-seat A-10 Night Adverse Weather (N/AW) version was built by converting an A-10A.^[7] The Night Adverse Weather (N/AW) aircraft was developed by Fairchild from the first Demonstration Testing and Evaluation (DT&E) A-10 for consideration by the USAF. It included a second seat for a weapons system officer responsible for ECM, navigation and target acquisition. The variant was canceled and the only two-seat A-10 built now sits at Edwards Air Force Base awaiting a spot in the Flight Test Historical Foundation museum.^[8] The proposed two-seat A-10 trainer aircraft did not go into production, as it was felt that the A-10 was simple enough to fly that a trainer version would not be required.

The decision to make the 30 mm GAU-8 gun the main anti-tank weapon of the A-X was influenced by Vietnam era A-1 pilots and by Hans-Ulrich Rudel and his book, "Trotzdem" (Released in the U.S. as a substantially edited version under the name "Stuka Pilot"). In World War II, Rudel flew the Ju 87G Stuka for the Luftwaffe and destroyed many Soviet tanks using its two underwing Bordkanone BK 3.7 37 mm caliber anti-tank autocannon. His book was required reading for members on the A-X project. The Ju 87G was an outmoded airframe with improvised anti-tank weapons attached, yet still inflicted significant casualties on Soviet tank forces.

[edit] Upgrades

The A-10 has received many upgrades over the years. Aircraft were upgraded with inertial navigation and a Pave Penny laser sensor (marked target seeker) pod that allowed the pilot to detect laser energy for PID (Positive Identification) of an illuminated target. The Pave Penny is a passive seeker and cannot self-designate a target for a Laser Guided Bomb (LGB). Later, the Low-Altitude Safety and Targeting Enhancement (LASTE) upgrade provided computerized weapon-aiming equipment, an autopilot, and ground-collision warning system. The A-10 is now compatible with night vision goggles for low-light operation. In 1999, aircraft began to receive Global Positioning System navigation systems, and in 2005 began getting its LASTE system upgraded with the Integrated Flight & Fire Control Computers (IFFCC).

In 2005, the entire A-10 fleet also began receiving upgrades that would result in redesignation to the "C" model that will include improved fire control system (FCS), electronic countermeasures (ECM), and the ability to carry smart bombs. The A-10 will be part of a service life extension program (SLEP) with many receiving new wings.^[9] A contract to build 242 new A-10 wing sets was awarded to Boeing on 29 June 2007.^[10] Modifications to provide precision weapons capability are well underway. The Air Force Material Command's Ogden Air Logistics Center at Hill AFB, Utah completed work on its 100th A-10 precision engagement upgrade in January 2008.^[11] The C model upgrades are to be completed in 2011.^[12]

On 2 April 2007 the Government Accounting Office estimated the potential total cost of upgrading, refurbishing, and service life extension plans for the A-10 force at up to $4.4 billion.^[13]

[edit] Design

The A-10 has superior maneuverability at low speeds and altitude, thanks to large wing area, high wing aspect ratio, and large ailerons. The large high aspect ratio wing also allows for short takeoffs and landings, permitting operations from rugged, forward airfields near front lines. The aircraft can loiter for extended periods of time and operate under 1,000 feet (300 m) ceilings with 1.5-mile (2.4 km) visibility. It typically flies at a relatively slow speed of 300 knots (345 mph or 555 km/h), which makes it a much better platform for the ground-attack role than fast fighter-bombers, which often have difficulty targeting small and slow-moving targets.

Engine exhaust passes over the aircraft's horizontal stabilizer and between the twin tails, decreasing the A-10's infrared signature and lowering the likelihood that the aircraft can be targeted by heat-seeking missiles. The placement of the engines behind the wings partially shields them from anti-aircraft fire. The leading edge of the wing is honeycomb to provide strength with minimal weight compromise. Honeycomb panels of this type on the A-10 include the flap shrouds, elevators, rudders and other sections of the fins.

The A-10 has integrally machined skin panels. Because the stringers are integral with the skin there are no join or seal problems. These panels, fabricated using computer controlled machining, reduce the time and hence the cost of production. Combat experience has shown that this type of panel is more resistant. The skin is not load-bearing, so damaged skin sections can be easily replaced in the field, with makeshift materials if necessary.^[14]

The ailerons are at the far ends of the wings to gain greater rolling moment as with most aircraft but there are two distinguishing features. First, the ailerons are larger than is typical, almost 50% of the chord, providing improved control even at slow speeds. The aileron is also split, making it a deceleron.

The Thunderbolt II can be serviced and operated from bases with limited facilities near battle areas. An unusual feature is that many of the aircraft's parts are interchangeable between the left and right sides, including the engines, main landing gear, and vertical stabilizers. The sturdy landing gear, low-pressure tires and large, straight wings allow operation from short rough strips even with a heavy ordnance load, allowing the aircraft to operate from damaged airbases. If runways are damaged in an attack, the A-10 can operate from taxiways, or straight roadway sections, such as Germany's autobahn.^[15] The aircraft is designed to be refueled, rearmed, and serviced with minimal equipment. Operating from a forward area is both useful for close air support and necessary due to the A-10's relatively low cruise and top speeds.

Because of the close proximity of the front landing gear and the A-10's main cannon, the landing gear is offset to the aircraft's right and cannon slightly to the left (see schematic below). During ground taxi, the offset front landing gear causes the A-10 to have dissimilar turning radii. Turning to the right on the ground takes less space than turning left.^[16]

[edit] Durability

The A-10 is exceptionally hardy. Its strong airframe can survive direct hits from armor-piercing and high-explosive projectiles up to 23 mm. The aircraft has triple redundancy in its flight systems, with mechanical systems to back up double-redundant hydraulic systems. This permits pilots to fly and land when hydraulic power or part of a wing is lost. Flight without hydraulic power uses the manual reversion flight control system; this engages automatically for pitch and yaw control, and under pilot control (manual reversion switch) for roll control. In manual reversion mode, the A-10 is sufficiently controllable under favorable conditions to return to base and land, though control forces are much higher than normal. The aircraft is designed to fly with one engine, one tail, one elevator and half a wing torn off.^[17] Self-sealing fuel tanks are protected by fire-retardant foam. Additionally, the main landing gear is designed so that the wheels semi-protrude from their nacelles when the gear is retracted so as to make gear-up landings (belly landing) easier to control and less damaging to the aircraft's underside. A belly landing would be required in the case of a landing gear failure; for other jets, the only options would be a water landing, or a rough, risky landing on the aircraft's underside, engine(s), or external fuel tanks. Also, the A-10's landing gear are all hinged toward the rear of the aircraft, so if hydraulic power is lost the pilot can simply drop the gear and a combination of gravity and wind resistance will open and lock the gear in place.

The cockpit and parts of the flight-control system are protected by 900 pounds (408 kg) of titanium armor, referred to as a titanium "bathtub".^[18] The tub has been tested to withstand strikes from 23 mm cannon fire and some strikes from 57 mm rounds.^[18] It is made up of titanium plates with thicknesses from ½ inch to 1½ inches determined by a study of likely trajectories and deflection angles. This protection comes at a cost, though; the armor itself weighs almost 6% of the entire aircraft’s empty weight. To protect the pilot from the fragmentation likely to be created from impact of a shell, any interior surface of the tub that is directly exposed to the pilot is covered by a multi-layer Kevlar spall shield. The canopy consists of a bullet-proof diffusion-bonded stretched-acrylic to withstand small arms fire and is resistant to spalling. The front windscreen offers shielding resistant to 20 mm cannon fire.

Recent proof of the durability of the A-10 was shown when then-Captain Kim Campbell, USAF, flying a ground support mission over Baghdad during the 2003 invasion of Iraq, suffered extensive flak damage to her A-10. Enemy fire damaged one of the A-10's engines and crippled its hydraulic system, forcing the back-up mechanical system to operate the aircraft's stabilizer and flight controls. Despite this, Campbell managed to fly it for an hour and landed it safely at the air base in manual reversion mode.

[edit] Powerplant

There are several reasons for the unusual location of the A-10's General Electric TF34-GE-100 turbofan engines. First, the A-10 was expected to fly from forward air bases, often with semi-prepared substandard runways that presented a high risk of foreign object damage to the engines. The height of the engines lowers the chance that sand or stones will enter the inlet. This also allows engines to remain running, allowing for shorter servicing and rearming turn-around times by ground crew. Servicing and rearming are further helped by having wings closer to the ground than would be possible if the engines were wing-mounted. The position also reduces the IR signature further, which is already low due to the engines' 6:1 bypass ratio. Because of their high position, the engines are angled upward nine degrees to bring the combined thrust line closer to the aerodynamic center of the aircraft. This avoids trimming measures to counteract a nose-down pitching moment if the engines were parallel to the fuselage. The heavy engines require strong supports, so their pylons are connected to the airframe by four bolts.^[19]

All four fuel tanks are near the center of the aircraft, reducing the likelihood that they will be hit or separated from the engines. The tanks are protected by several measures. The tanks are separate from the fuselage; thus, projectiles would need to penetrate the skin before reaching the tank. The refueling system is purged after use so that there is no fuel unprotected anywhere in the aircraft. All pipes self-seal if they are compromised. Most of the fuel system components are inside the tanks so that if a leak were to occur from the component the fuel would not be lost. If a tank does get damaged, check valves ensure that fuel does not flow into the compromised tank. Most importantly, reticulated polyurethane foam lines both the inner and outer sides of the fuel tanks, holding debris and restricting fuel spillage in the event of damage. The other source of possible combustion, the engines, are shielded from the fuel system and the rest of the airframe by firewalls and fire extinguishing equipment.

[edit] Weapon systems

Although the A-10 can carry considerable disposable stores, its primary built-in weapon is the 30 mm GAU-8/A Avenger Gatling gun. One of the most powerful aircraft cannons ever flown, it fires large depleted uranium armor-piercing shells. In the original design, the pilot could switch between two rates of fire: 2,100 or 4,200 rounds per minute;^[20] this was changed to a fixed rate of 3,900 rounds per minute.^[21] The cannon takes about half a second to come up to speed, so 50 rounds are fired during the first second, 65 or 70 rounds per second thereafter. The gun is precise; it can place 80% of its shots within a 40-foot (12.4 m) circle from 4,000 feet (1,220 m) while in flight.^[22] The GAU-8 is optimized for a slant range of 4,000 feet (1,220 m) with the A-10 in a 30 degree dive.^[23]

The fuselage of the aircraft is built around the gun.^[24] For example, the nose wheel is offset to the right so that the gun's firing barrel at the 9 o'clock position is aligned on the aircraft's centerline. The gun's ammunition drum can hold up to 1,350 rounds of 30 mm ammunition,^[25] but generally holds 1,174 rounds.^[23] The damage caused by rounds firing prematurely due to impact of an explosive shell would be catastrophic, so a great deal of effort has been taken to protect the 5 feet 11.5 inches (1.82 m) long drum.^[25] There are many armor plates of differing thicknesses between the aircraft skin and the drum, to detonate an incoming shell before it reaches the drum. A final layer of armor around the drum itself protects it from fragmentation damage. The gun is loaded by Syn-Tech's linked tube carrier GFU-7/E 30 mm ammunition loading assembly cart; a vehicle unique to the A-10 and GAU-8.

Another commonly used weapon is the AGM-65 Maverick air-to-surface missile, with different variations for either electro-optical (TV-guided) or infra-red targeting. The Maverick allows targets to be engaged at much greater ranges than the cannon, a safer proposition in the face of modern anti-aircraft systems. During Desert Storm, in the absence of dedicated forward-looking infrared cameras, the Maverick's infra-red camera was used for night missions as a "poor man's FLIR". Other weapons include cluster bombs and Hydra rocket pods. Although the A-10 is equipped to deliver laser-guided bombs, their use is relatively uncommon; at the low altitudes and speeds of typical A-10 operations, standard unguided bombs provide adequate accuracy at far lower cost. In any event, the guided weapons would provide little benefit, as there would be nearly no time for the weapons to steer onto a target. A-10s usually fly with an ALQ-131 ECM pod under one wing and two AIM-9 Sidewinder air-to-air missiles under the other wing for self-defense.

[edit] Modernization

The A-10 Precision Engagement Modification Program will update 356 A-10/OA-10s to the A-10C variant with a new flight computer, new glass cockpit displays and controls, two new 5.5-inch (140 mm) color displays with moving map function and an integrated digital stores management system.^[26][27]

Other funded improvements to the A-10 fleet include a new data link, the ability to employ smart weapons such as the JDAM and Wind Corrected Munitions Dispensor, and the ability to carry an integrated targeting pod such as the Northrop Grumman LITENING targeting pod or the Lockheed Martin Sniper XR Advanced Targeting Pod (ATP). Also included is the ROVER or remotely operated video enhanced receiver to provide sensor data to personnel on the ground.^[12]

[edit] Operational history

The first unit to receive the A-10 Thunderbolt II was the 355th Tactical Training Wing, based at Davis-Monthan Air Force Base, Arizona in March 1976. The first unit to achieve full combat-readiness was the 354th Tactical Fighter Wing at Myrtle Beach AFB, South Carolina in 1978. Deployments of A-10As followed at bases both at home and abroad, including England AFB, Louisiana, Eielson AFB, Alaska, Osan Air Base, South Korea, and RAF Bentwaters/RAF Woodbridge, England. The 81st TFW of RAF Bentwaters/RAF Woodbridge operated rotating detachments of A-10s at four bases in Germany known as Forward Operating Locations (FOLs): Leipheim, Sembach Air Base, Nörvenich, and Ahlhorn.^[28]

A-10s were initially an unwelcome addition to the arsenal in the eyes of Air Force brass. As the Air Force senior leadership became increasingly populated by general officers from the fighter community, the Air Force prized the high-flying, high-performance F-15 Eagle and F-16 Fighting Falcon fighter jets, and were determined to leave close air support primarily to Army helicopters.

The A-10 saw combat for the first time during the Gulf War in 1991, destroying more than 900 Iraqi tanks, 2,000 military vehicles, and 1,200 artillery pieces. A-10s shot down two Iraqi helicopters with the GAU-8 gun.^[6] The first of these occurred on February 6, 1991 when Captain Robert Swain shot down an Iraqi helicopter over Kuwait marking the A-10's first air-air victory.^[29] Four A-10s were shot down during the war, all by surface-to-air missiles.^[30] A-10s had a mission capable rate of 95.7%, flew 8,100 sorties, and launched 90% of the AGM-65 Maverick missiles fired in the conflict.^[31] Shortly after the Gulf War, the Air Force gave up on the idea of replacing the A-10 with a close air support version of the F-16.^[32]

In the 1990s many A-10s were shifted to the forward air control (FAC) role and redesignated OA-10. In the FAC role the A-10 is typically equipped with up to six pods of 2.75 inch (70 mm) Hydra rockets, usually with smoke or white phosphorus warheads used for target marking. OA-10s remain fully combat capable despite the redesignation.

A-10s again saw service in the 1999 Kosovo War, in the later stages of the 2001 war in Afghanistan, during Operation Anaconda in March 2002 and in the Iraq war (2003-present).

On 30 April 2003, United States Air Forces Central issued Operation Iraqi Freedom: By the Numbers, a declassified report about the aerial campaign in the conflict. Sixty A-10s were deployed in Iraq; one was shot down near Baghdad International Airport by Iraqi fire late in the campaign. Of the A-10s deployed, 47 were Air National Guard aircraft, and 12 were from the Air Force Reserve. The A-10 had a mission capable rate of 85% in the war, and fired 311,597 rounds of 30 mm ammunition. The A-10 also flew 32 missions in which the aircraft dropped propaganda leaflets over Iraq.^[33]

The A-10C first deployed to Iraq in the third quarter of 2007 with the 104th Fighter Squadron of the Maryland Air National Guard. The jets include the Precision Engagement Upgrade.^[34] The A-10C's digital avionics and communications systems have greatly reduced the time to acquire a close air support target and attack it.^[35]

The A-10 is scheduled to stay in service with the USAF until 2028 and possibly later,^[36] when it may be replaced by the F-35 Lightning II.^[9] The A-10 fleet is currently undergoing upgrades.

[edit] Variants

YA-10A 

Pre-production variant. Two were built.

A-10A 

Single-seat close air support, ground-attack version.

OA-10A 

A-10As used for airborne forward air control.

YA-10B Night/Adverse Weather

Two-seat experimental prototype, for work at night and in bad weather. Later redesignated YA-10B. The one prototype was a A-10A conversion and is now on static display.

A-10C 

A-10As updated under the incremental Precision Engagement (PE) program.

[edit] Operators

The A-10 has been flown exclusively by the United States Air Force and its Air Reserve Components, the Air Force Reserve Command (AFRC) and the Air National Guard (ANG). The USAF operated a total of 353 A-10 and OA-10 aircraft (196 in active duty, 106 in ANG, and 51 in AFRC, all variants) as of September 2007.^[37]

As of 2008, 20 squadrons operate the A-10 or its OA-10 variant (nine USAF, six ANG, and five AFRC).

United States Air Force

• 23d Wing: Moody Air Force Base, Georgia
  • 74th Fighter Squadron
  • 75th Fighter Squadron
• 51st Fighter Wing: Osan Air Base, South Korea
  • 25th Fighter Squadron
• 52d Fighter Wing: Spangdahlem Air Base, Germany
  • 81st Fighter Squadron
• 53d Wing: Eglin Air Force Base, Florida
  • 422d Test and Evaluation Squadron (Nellis Air Force Base, Nevada)
• 57th Wing: Nellis AFB, Nevada
  • 66th Weapons Squadron
• 355th Wing: Davis-Monthan Air Force Base, Arizona
  • 354th Fighter Squadron
  • 357th Fighter Squadron
  • 358th Fighter Squadron

Air National Guard

• 110th Fighter Wing: Battle Creek ANGB, Michigan (BRAC 2005 moves most, but not all, A-10 aircraft to 107th Fighter Squadron at Selfridge ANGB, Michigan)
  • 172d Fighter Squadron
• 111th Fighter Wing: NAS JRB Willow Grove/Willow Grove ARS, Pennsylvania (BRAC 2005 currently sees unit losing aircraft in 2012)
  • 103d Fighter Squadron
• 124th Wing: Boise Air Terminal, Idaho
  • 190th Fighter Squadron
• 175th Wing: Warfield ANGB, Martin State Airport, Maryland
  • 104th Fighter Squadron
• 188th Fighter Wing: Fort Smith, Arkansas (Transitioned from F-16s to A-10s due to BRAC 2005)

Air Force Reserve Command

• 442d Fighter Wing: Whiteman Air Force Base, Missouri
  • 76th Fighter Squadron (Geographically Separated Unit (GSU) at Moody AFB, Georgia)
  • 303d Fighter Squadron
• 917th Wing: Barksdale Air Force Base, Louisiana
  • 45th Fighter Squadron (GSU at Davis-Monthan Air Force Base, Arizona)
  • 47th Fighter Squadron

[edit] Former Operators

United States Air Force

• • 355th Fighter Squadron: part of current 354th Fighter Wing, Eielson Air Force Base, [[Alaska] (squadron inactivated 2007)

Air Force Reserve Command

• 926th Fighter Wing: NAS JRB New Orleans, Louisiana
  • 706th Fighter Squadron (wing and squadron deactivated 2007 due to BRAC 2005)

Air National Guard

• 103d Fighter Wing: Bradley ANGB, Connecticut (BRAC 2005 removed A-10 aircraft, redesignated as 103d Airlift Wing and given C-21 in 2007)
  • 118th Fighter Squadron (resdesignated 118th Airlift Squadron per BRAC 2005)
• 104th Fighter Wing: Barnes ANGB, Massachusetts (BRAC 2005 saw unit transition from A-10 to F-15C in 2007)
  • 131st Fighter Squadron

[edit] Specifications (A-10A)

Data from The Great Book of Modern Warplanes,^[38] Fairchild-Republic A/OA-10^[39]

General characteristics

• Crew: 1
• Length: 53 ft 4 in (16.26 m)
• Wingspan: 57 ft 6 in (17.53 m)
• Height: 14 ft 8 in (4.47 m)
• Wing area: 506 ft² (47.0 m²)
• Airfoil: NACA 6716 root, NACA 6713 tip
• Empty weight: 24,959 lb (11,321 kg)
• Loaded weight:
  
  • Standard: 30,384 lb (13,782 kg)
  • On CAS mission: 47,094 lb (21,361 kg)
  • On anti-armor mission: 42,071 lb (19,083 kg)
• Max takeoff weight: 50,000 lb (23,000 kg)
• Powerplant: 2× General Electric TF34-GE-100A turbofans, 9,065 lbf (40.32 kN) each

Performance

• Never exceed speed: 450 knots (518 mph,^[39] 833 km/h) at 5,000 ft (1,500 m) with 18 Mk 82 bombs^[40]
• Maximum speed: 381 knots (439 mph, 706 km/h) at sea level, clean^[39]
• Cruise speed: 300 knots (340 mph, 560 km/h)
• Stall speed: 120 knots (220 km/h) ^[41]
• Combat radius:
  
  • On CAS mission: 250 nmi (288 mi, 460 km) at 1.88 hour single-engine loiter at 5,000 ft (1,500 m), 10 min combat
  • On anti-armor mission: 252 nmi (290 mi, 467 km), 40 nm (45 mi, 75 km) sea-level penetration and exit, 30 min combat
• Ferry range: 2,240 nmi (2,580 mi, 4,150 km) with 50 knot (55 mph, 90 km/h) headwinds, 20 minutes reserve
• Service ceiling: 45,000 ft (13,700 m)
• Rate of climb: 6,000 ft/min (30 m/s)
• Wing loading: 99 lb/ft² (482 kg/m²)
• Thrust/weight: 0.36

Armament

• Guns: 1× 30 mm (1.18 in) GAU-8/A Avenger gatling cannon with 1,174 rounds
• Hardpoints: 11 (8× under-wing and 3× under-fuselage pylon stations) with a capacity of 16,000 lb (7,260 kg),with provisions to carry combinations of:
  • Rockets:
    
    • 4× LAU-61/LAU-68 rocket pods (each with 19× / 7× Hydra 70 mm rockets, respectively)
    • 4× LAU-5003 rocket pods (each with 19× CRV7 70 mm rockets)
    • 6× LAU-10 rocket pods (each with 4× 127 mm (5.0 in) Zuni rockets)
  • Missiles:
    
    • 2× AIM-9 Sidewinders air-to-air missiles for self-defense
    • 8× AGM-65 Maverick air-to-surface missiles
  • Bombs:
    
    • Mark 80 series of unguided iron bombs or
    • Mk 77 incendiary bombs or
    • BLU-1, BLU-27/B Rockeye II, Mk20, BL-755^[42] and CBU-52/58/71/87/89/97 cluster bombs or
    • Paveway series of Laser-guided bombs or
    • Joint Direct Attack Munition (A-10C)^[43] or
    • Wind Corrected Munitions Dispenser (A-10C)*SUU-42A/A Flares/Infrared decoys dispenser pod and chaff pod or
• AN/ALQ-131 & AN/ALQ-184 ECM pods or
• Lockheed Martin Sniper XR & LITENING targeting pods (A-10C) or
• 2× 600 US gallon Sargent Fletcher drop tanks for extended range/loitering time.

Avionics

• Pave Penny laser tracker pod (mounted beneath right side of cockpit) for use with Paveway LGBs

[edit] Nicknames

The A-10 Thunderbolt II received its popular nickname "Warthog" from the pilots and crews of the USAF attack squadrons who flew and maintained it. The A-10 is the last of Republic's jet attack aircraft to serve with the USAF. The Republic F-84 Thunderjet was nicknamed the "Hog", F-84F Thunderstreak nicknamed "Superhog", and the Republic F-105 Thunderchief tagged "Ultra Hog".^[3] A less common nickname is the "Tankbuster".^[44]

[edit] See also

• Craig D. Button
• 190th Fighter Squadron, Blues and Royals friendly fire incident
  

Comparable aircraft

• Northrop YA-9
• Sukhoi Su-25
  

Related lists

• List of attack aircraft
• List of active United States military aircraft
• List of friendly fire incidents
  

[edit] References

[edit] Notes

[edit] Bibliography

[edit] External links

Wikimedia Commons has media related to: A-10 Thunderbolt II

• USAF A-10 fact sheet page
• A-10.org web site
• A-10 web page on GlobalSecurity.org
• A-10 web page on f as.org
• The Warthog Pen web site
• A-10 Battle Damage Repair Gulf War
• Republic A-10 Construction—National Museum of the United States Air Force fact sheet page
• Republic A-10A—National Museum of the United States Air Force fact sheet page
• Republic Night/Adverse Weather A-10—National Museum of the United States Air Force fact sheet page

v • d • e Aircraft produced by Fairchild Aircraft, subsidiaries, and successor companies Manufacturer designations FC-1 • FC-2 KR-21 • KR-31 • KR-34 • KR-125 • KR-135 21 • 22 • 24 • 41 • 42 • 45 • 46 • 51 • 61 • 62 • 71 • 72 • 78/78 • 81 • 82 • 84 • 91 • 100 • 135 • 140 • 150 By role Passenger transports: FC-1 • FC-2 • 21 • 22 • 24 • 41 • 42 • 45 • 46 • 51 • 71 • 72 • 81 • 82 • 91 • 92 • 100 • 135 • 140 • 150 Military trainers: AT-21 • PT-19 • PT-23 • PT-26 • XNQ Military transports and utility aircraft: C-82 • C-119 • C-123 • C-26 Fairchild (Canada) 34-42 • 45-80 • 51/71 • F-11 • Super 71 Fairchild-Dornier Do 228 • 328 • 328JET Fairchild Hiller F-27/FH-227 • FH-1100 Fairchild Republic A-10 • T-46 Fairchild Swearingen Merlin • Metroliner Under license US: AU-23 Canada: Handley Page Hampden • Bristol Fairchild Bolingbroke • SBF Helldiver

v • d • e United States tri-service attack aircraft designations post-1962 A-1 • A-2 • A-3 • A-4 • A-5 • A-6 • A-7 • (A-8 not assigned) • YA-9 • A-10 • (A-11 not assigned) • A-12 See also: A-26 (redesignated from B-26) • A-37 (redesignated from AT-37) • AV-8A/AV-8B (attack aircraft designated under the "V" for V/STOL sequence)

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v • d • e Current United States Air Force Weapons Systems Aircraft Attack A/OA-10A/C Thunderbolt II · AC-130H/U Spectre/Spooky II Bomber B-1B Lancer · B-2A Spirit · B-52H Stratofortress Electronic Warfare E-3B/C Sentry · E-4B · E-8C Joint STARS · E-9A · EC-130J Commando Solo Fighter F-15C/D Eagle · F-15E Strike Eagle · F-16C/D Fighting Falcon · F-22A Raptor Reconnaissance OC-135B Open Skies · RC-26B · RC-135S/U/V/W · RQ-4A Global Hawk · RQ-11B Raven · U-2R/S Dragon Lady · WC-130J Super Hercules · WC-135C/W Constant Phoenix · Scan Eagle · WASP-III Search and Rescue HH-60G/MH-60G Pave Hawk  · HC-130P/N Tanker KC-10A Extender · KC-135E/R/T Stratotanker Trainer T-1A Jayhawk · T-6A Texan II · T-37B Tweet · (A)T-38A/B/C Talon · T-43A · TG-10B/C/D · TG-15A/B Transport C-5A/B/C/M Galaxy · VC-9C · C-12C/D/F Huron · C-17A Globemaster III · C-20A/B/C Gulfstream III · C-20G/H Gulfstream IV · C-21A Learjet · CV-22 Osprey · VC-25A · C-32A/B · C-37A Gulfstream V · C-37B Gulfstream V · C-38 Courier · C-40B Clipper · C-41A Aviocar · C-130E/H/J Hercules Utility/Multi-Mission LC-130H · MC-130 Combat Talon I,II/Combat Spear/Combat Shadow · MQ-1B Predator · MQ-9 Reaper · U-28A · UH-1H/N/V Huey · UV-18A/B Twin Otter · YAL-1 C2 AN/USQ-163 Falconer Munitions Bomb CBU-87 Combined Effects Munition · CBU-89 Gator · CBU-97 Sensor Fuzed Weapon · GBU-10 Paveway II · GBU-12 Paveway II · GBU-15 · GBU-24 Paveway III · GBU-27 Paveway III · GBU-28 · GBU-31 JDAM · GBU-32 JDAM · GBU-38 JDAM · GBU-39 Small Diameter Bomb · GBU-54 Laser JDAMMk-82 · Mk-84 · M129 Missile AGM-65A/B/D/E/G/G2/H/K Maverick · AGM-86B/C/D Air-Launched Cruise Missile (ALCM) · AGM-88A/B/C High-speed Anti-radiation Missile (HARM) · AGM-130 Powered Standoff Weapon · AGM-154A Joint Standoff Weapon (JSOW) · AGM-158 Joint Air-to-Surface Stand-off Missile (JASSM) · AIM-7M Sparrow · AIM-9M/X Sidewinder · AIM-120B/C Advanced Medium-Range Air-to-Air Missile (AMRAAM) · LGM-30G Minuteman III Target BQM-34 Firebee · BQM-167 Subscale Aerial Target · MQM-107 Streaker · QF-4 Aerial Target Small Arms M4 Carbine · M9 Semiautomatic Pistol · M11 Semiautomatic Pistol · M1911A1 Semiautomatic Pistol · M14 Stand-off Munitions Disruptor (SMUD) · M16A2 Rifle · M18A1 Claymore Mine · M24 Sniper Weapon System · M67 Fragmentation Grenade · M79 Grenade Launcher · M107/M82A1 Long Range Sniper Rifle · M2 .50-Caliber Machine Gun · M240B Medium Machine Gun · M249 light machine gun · M60 Medium Machine Gun · MCS 870 Modular Combat Shotgun · MK-19 40 mm Machine Gun · MP5K Submachine Gun · UZI Submachine Gun · M72 Light Anti-tank Weapon (LAW) · Shotgun · GAU-5A/GUU-5P Carbine · M136 AT4 Light Anti-tank Weapon · Mk 14 Mod 0 Enhanced Battle Rifle Space Systems Launch Vehicle Atlas V · Delta II · Delta IV Satellite Defense Meteorological Satellite Program (DMSP) · Defense Satellite Communications System (DSCS) · Defense Support Program (DSP) · Global Positioning System (GPS) · Milstar Satellite Communications System · Space-Based Infrared System (SBIRS) · Wideband Global SATCOM