F-111 - EF-111 @·AIRCRAFTUBE

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  • General Dynamics F-111 AFTI NASA General Dynamics F-111 AFTI NASA
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  • General Dynamics EF-111A Raven General Dynamics EF-111A Raven
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  • EF-111 Raven EF-111 Raven
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  • General Dynamics F-111 TACT General Dynamics F-111 TACT
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  • F-111A Combat Lancer - 1968 F-111A Combat Lancer - 1968
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General Dynamics F-111 & EF-111

The General Dynamics F-111 is a medium-range strategic bomber, reconnaissance, and tactical strike aircraft designed in the 1960s. The United States Air Force (USAF) variants were officially named "Aardvark ", their longtime nickname, at their ceremony of retirement from service in 1996. The last operator of the F-111 was the Royal Australian Air Force (RAAF), and in Australian service the F-111 was known as the "Pig".

The F-111 pioneered several technologies for production military aircraft, including variable-geometry wings, afterburning turbofan engines, and terrain following radar for low-level, high-speed flight. Its design was highly influential, particularly for Soviet engineers, and some of its advanced features have since become commonplace. In its inception, however, the F-111 suffered a variety of development problems, and several of its intended roles, such as naval interception, failed to materialize.

In USAF service the F-111 has been effectively replaced by the F-15E Strike Eagle for medium-range precision strike missions, while the supersonic bomber role has been assumed by the B-1B Lancer.

Development

The beginnings of the F-111 were in the TFX program, an ambitious early 1960s project to combine the U.S. Air Force requirement for a fighter-bomber with the U.S. Navy 's need for a long-range carrier defense fighter to replace the F-4 Phantom II and the F-8 Crusader. The fighter design philosophy of the day concentrated on very high speed, raw power, and air-to-air missiles.

Air Force specifications

The USAF's Tactical Air Command (TAC) was largely concerned with the fighter-bomber and deep strike/interdiction roles, which in the early 1960s still focused on the use of nuclear weapons. The aircraft would be a follow-on to the F-105 Thunderchief, which was designed to deliver nuclear weapons low, fast and far. Air combat would be an afterthought until encountering MiGs over Vietnam in the mid 1960s. In June 1960 the USAF issued a specification for a long-range interdiction/strike aircraft able to penetrate Soviet air defenses at very low altitudes and very high speeds to deliver tactical nuclear weapons against crucial Soviet targets like airfields and supply depots. Included in the specification were a low-level speed of Mach 1.2, a high-altitude speed of Mach 2.5, a combat radius of 890 miles (or 1,430 km), good short-field performance, and a ferry range long enough to reach Europe without refuelling.

Navy requirement

Meanwhile the US Navy had, since 1957, been searching for a long-range, high-endurance interceptor to defend its carrier groups against the new generation of Soviet jet bombers, which by then were being armed with huge anti-ship missiles with nuclear warheads. The Navy needed a Fleet Air Defense (FAD) aircraft with better loitering performance and load-carrying ability than the F-4 Phantom II, and one equipped with a powerful radar and a battery of long-range missiles to intercept both bombers and their missiles.

The Navy had studied, but rejected, a slow straight-winged missile carrier, the F6D Missileer. In December 1960 the Navy had been reconsidering variable geometry for the FAD requirement. The trend toward ever bigger, more powerful fighters posed a problem for the Navy: the current generation of naval fighters were already barely capable of landing on an aircraft carrier deck, and a still larger and faster fighter would pose even greater problems. An airframe optimized for high-speed - most obviously with a high-angle swept wing - is inefficient at cruising speeds, which reduces range, payload, and endurance, and leads to very high landing speeds. On the other hand, an airframe with a straight or modestly swept wing, while easier to handle and able to carry heavy loads over longer distances on a minimum of fuel, has lower ultimate performance. Variable geometry, which the Navy had tried and abandoned for the XF10F Jaguar in 1953, offered the possibility of combining both in a single airframe.

Similar swing wing aircraft

The F-111 was the first production variable-geometry aircraft. The earlier subsonic Navy XF10F Jaguar had been cancelled in 1953. It inspired a number of aircraft throughout the 1980s, and even fictional aircraft on the Thunderbirds, but swing wings are extinct in newer designs due to higher cost, and the extra weight imposed by the swing wing mechanism. Nevertheless, several other types have followed, including the Soviet Sukhoi Su-17 'Fitter' (1966), Mikoyan-Gurevich MiG-23 'Flogger' (1967), Tupolev Tu-22M 'Backfire' (1969) and Tupolev Tu-160 'Blackjack' (1981), the U.S. F-14 Tomcat naval fighter (1970) and B-1 Lancer bomber (1974), and the European Panavia Tornado (1974). The Sukhoi Su-24 'Fencer' (1970), which resembles the F-111, also has side-by-side seating.

Armament

Although conceived as a multi-role fighter, the F-111 became a long-range attack aircraft primarily armed with air-to-surface ordnance.

Weapons bay

The F-111 has a small internal weapons bay under the fuselage for various weapons. Cannon: All tactical combat versions (that is, not the EF-111A or FB-111A/F-111G) could carry a single M61 Vulcan 20 mm cannon with a very large (2,084 round) ammunition tank, covered by an eyelid shutter when not in use. Although carried by some USAF aircraft, the cannon was never actually used in combat, and was removed by the early 1980s; provision for the cannon has also been deleted from Australian F-111Cs.

Bombs: The bay can alternately hold two conventional bombs, usually the Mk 117 type of nominal 750 lb/340 kg weight, although weapons up to the Mk 118 (3,000 lb/1,400 kg) were cleared.

Nuclear weapons: All F-111 models except the EF-111A and the Australian F-111C were equipped to carry various free-fall nuclear weapons: tactical models generally carried the B43, B57, or B61, the FB-111A those weapons or the B83. The FB-111A could also carry one or two AGM-69 SRAM nuclear missiles in its weapons bay.

Sensor pod: The F-111C and F-111F were equipped to carry the AN/AVQ-26 Pave Tack targeting system on a rotating carriage that kept the pod protected within the weapons bay when not in use. Pave Tack is a FLIR and laser rangefinder /designator that allows the F-111 to designate and drop laser-guided bombs.

Reconnaissance pallet: Australian RF-111Cs carry a package of reconnaissance sensors and cameras for tactical recce missions. It contains two video cameras, a Honeywell AN/AAD-5 infrared linescan (recorded on video or film), a Fairchild KA-56E low-altitude and KA-93A4 high-altitude panoramic cameras, and a pair of CAI KS-87C split vertical cameras. It can also record photographs of the attack radar's display.

Missiles: The F-111B was intended to be capable of carrying two AIM-54 Phoenix air-to-air missiles in the bay. General Dynamics proposed an arrangement that would allow two AIM-9 Sidewinders to be carried on a trapeze mounting in the bay (at the expense of the M61 cannon), along with a single (usually nuclear) bomb. This was not adopted, with the USAF and RAAF opting for the cannon instead. The AIM-7 Sparrow or AIM-4 Falcon, standard on the F-4, was never fitted, though later F-111 models had radars equipped to guide the Sparrow. Other equipment: Auxiliary fuel tanks and baggage pods were sometimes carried.

External ordnance

The design of the F-111's fuselage prevents the carriage of external weapons under the fuselage (although there are two small stations, one on the weapon bay, the other on the rear fuselage between the engines, for ECM pods and/or datalink pods for guided weapons). All aircraft have provision for eight underwing pylons, four under each wing, with a capacity of 6,000 lb (or 2,700 kg) each. The inner pylons (3, 4, 5, and 6) pivot with the wing, but only one on each side can be loaded at maximum sweep. The outer pylons (1, 2, 7, and 8) are fixed, and can be loaded only if the wings are spread at less than 26°, causing drag at takeoff angle. The outermost pylons (1 and 8) have never been used operationally, and the second pair of fixed pylons (2 and 7) are fitted only rarely, for the carriage of fuel tanks. FB-111/F-111G models have provision to jettison their empty pylons in flight, reducing drag.

The limited number of fully swiveling pylons restricts the F-111's maximum practical weapons load, since the aircraft cannot use all pylons with the wings fully swept. By contrast, aircraft such as the F-14 and Tornado can carry their maximum bomb loads with fully swept wings.

The primary external armament of USAF tactical F-111s included:

  • Free-fall GP bombs :
    • Mk.82 (500 lb or 227 kg).
    • Mk.83 (1,000 lb or 454 kg).
    • Mk.84 (2,000 lb or 907 kg).
    • Mk.117 (750 lb or 340 kg).
  • Cluster bombs :
    • BLU-109 (2,000 lb or 907 kg) hardened penetration bomb.
  • Paveway laser-guided bombs, including :
    • GBU-10 (2,000 lb or 907 kg).
    • GBU-12 (500 lb or 227 kg).
    • GBU-28, a very specialized 4,800 lb (or 2,200 kg) penetration bomb using spare naval gun barrels as casings, hastily developed for the Gulf War.
    • BLU-107 Durandal runway -cratering bomb.
    • GBU-15 electro-optical bomb (using a Mk.84 or BLU-109 penetration weapon with a TV or infrared TV seeker from an AGM-65 Maverick, with guidance via an AXQ14 or ZWS-1 datalink pod.
    • AGM-130 stand-off bomb (essentially a Mk 84 or BLU-109 with GBU-15 guidance and a rocket booster, making it a powered missile with a range of 40 miles (or 64 km).

Although all F-111s can carry laser-guided munitions, only those with Pave Tack (i.e., F-111F and Australian F-111C) are capable of self-designation. Others can drop laser-guided weapons only with the aid of another ground or air designator.

From the early 1980s onward, tactical F-111s were fitted with shoulder rails on the sides of the outboard swiveling pylon (designated stations 3A and 6A) for two AIM-9 Sidewinder air-to-air missiles for self-defense. The standard Sidewinder fit was the AIM-9P, rather than the more modern AIM-9L or AIM-9M, whose larger fins were not compatible with the shoulder rail. The RAAF has considered replacing the Sidewinder with ASRAAM.

FB-111As could carry the same conventional ordnance as their tactical brothers, but their wing pylons were more commonly used for either fuel tanks or strategic nuclear gravity bombs. Until the weapon was withdrawn in 1990, they could carry up to four AGM-69 SRAM nuclear missiles on the wing pylons, although two was the more normal fit.

Australian F-111Cs have been equipped to launch the AGM-84 Harpoon anti-ship missile, AGM-88 HARM anti-radiation missile, and the AGM-142 Popeye stand-off missile.

Service life

The Strategic Air Command had FB-111s in service from 1969 through 1990.

The F-111 was in service with the USAF from 1967 through 1998. It entered active service with the Royal Australian Air Force in 1973 and is currently scheduled to remain with the RAAF until 2010.

Variants

F-111A

The F-111A was the initial production version of the F-111. It had TF30-P-3 engines with 12,000 lbf (53 kN) dry and 18,500 lbf (82 kN) afterburning thrust and "Triple Plow I" variable intakes, providing a maximum speed of Mach 2.2 (or 1,450 mph or 2,300 km/h) at altitude. The -A's Mark I avionics suite included the General Electric AN/APQ-113 attack radar mated to a separate Texas Instruments AN/APQ-110 terrain-following radar under the nose and a Litton AJQ-20 inertial navigation and nav/attack system.

Total production of the F-111A was 158, including 17 preproduction aircraft that were later brought up to production standards.

The first production F-111s were delivered on 18 July, 1967 to the 428th, 429th and 430th Tactical Fighter Squadrons of the 474th Tactical Fighter Wing based at first out of Cannon AFB, New Mexico, which relocated in 1968 to Nellis AFB.

After early testing a detachment of six aircraft were sent in March 1968 to Southeast Asia for Combat Lancer testing in real combat conditions in Vietnam. In little over a month, three aircraft were lost and the combat tests were halted. It turned out that all three had been lost through malfunction (primarily with the terrain-following radar), not by enemy action. This caused a storm of political recrimination, with US senators denouncing Secretary of Defense McNamara 's judgment in procuring the aircraft.

Behind the scenes, lessons were being learned and fixes being applied, but it was not until July of 1971 that the 474 TFW was fully operational. Testing in 1969 had revealed that a contractor had been paying off inspectors to approve sub-standard work on structural wing components, and all aircraft had to have the component replaced at significant cost (since most F-111As had been already completed). More failures were found and corrected in the wing pivot forgings.

September 1972 saw the F-111 back in Southeast Asia, participating in the final month of Operation Linebacker and later the Operation Linebacker II aerial offensive against the North. F-111 missions did not require tankers or ECM support, and they could operate in weather that grounded most other aircraft. One F-111 could carry the bomb load of four F-4 Phantom IIs. The worth of the new planes was beginning to show, and over 4,000 combat F-111A missions were flown over Vietnam with only six combat losses.

In 1977 the remaining F-111As were transferred to the 366 TFW based at Mountain Home AFB, equipping the 389th and 391st TFS.

In 1982, four surviving F-111As were converted to F-111C standard and provided to Australia as attrition replacements. They were fitted with the longer-span wings and reinforced landing gear of the -C, and subsequently were almost indistinguishable from new-build F-111Cs. Some of the -As delivered to the RAAF were Vietnam veterans, purportedly still bearing the scars of anti-aircraft fire.

A total of 42 F-111As were converted as the EF-111A Raven for an electronic warfare tactical electronic jamming role. They can be distinguished from other -As by the equipment bulge atop their tails, a featuring leading to the nickname "Fat Tail."

Three pre-production aircraft were provided to NASA for various testing duties. One was fitted with a variable-camber wing as part of the Advanced Fighter Technology Integration program in the 1980s; it was retired to the United States Air Force Museum at Wright Patterson AFB in 1989.

Most of the unconverted surviving F-111As were retired in 1991 and mothballed at AMARC, Davis Monthan AFB.

F-111B

The F-111B was to be a fleet-defense fighter for the US Navy, fulfilling a long-standing naval requirement for a fighter capable of carrying heavy, long-range missiles to defend carriers from Soviet anti-ship missiles. The Navy had just cancelled the F6D Missileer, a concept for a slow, straight-winged jet with the advanced Hughes AN/AWG-9 pulse-Doppler radar, which could detect low flying targets among ground clutter, and lift eight new AIM-54 Phoenix long-range, air-to-air missiles, which could attack multiple aircraft simultaneously at ranges out to 100 miles. The concept was soon cancelled, but the F-111 offered a platform with the range, payload, and Mach 2 performance of a fighter to intercept targets quickly, but with swing wings and turbofan engines, it could also loiter on station for long periods. The F-111B would carry six Phoenix missiles, but have no gun or other short range armament. General Dynamics, having no experience with carrier-based aviation, partnered with Grumman for this version.

The F-111B was a compromise that attempted to reconcile the Navy's very different needs with an aircraft whose basic configuration was largely set by the USAF need for a supersonic strike aircraft, and those compromises would harm both versions. The side-by-side seating was preferred by the Navy from the Missileer. The B was shorter than the F-111A, to enable it to fit on carrier lifts, but had a longer wingspan (70 ft/21.3 m compared to 63 ft/19.2 m) for increased range and cruising endurance. Although the Navy had wanted a 48-inch (122 cm) radar dish for long range, they were forced to accept a 36-inch (91.4 cm) dish for compatibility. The Navy had requested a maximum take-off weight of 50,000 lb (22,686 kg), but Secretary of Defense McNamara forced them to compromise at 55,000 lb (24,955 kg). This weight goal proved to be overly optimistic, although later successful fighters such as the F-14 Tomcat and F/A-18E/F Super Hornet would also far exceed these target weights.

Excessive weight plagued the B throughout its development. Not only were prototypes far over the 55,000 lb (24,955 kg) limit, efforts to redesign the airframe only made matters worse. The excessive weight made the aircraft seriously underpowered. In landing configuration at carrier weights, the F-111B could not maintain level flight on one engine, which would be a major problem once committed to the approach. Worse, its visibility for carrier approach and landing were abysmal.

Requirements for the F-111B had been formulated before air combat over Vietnam in 1965 showed the Navy still had a need for an aircraft which could engage MiG fighters at close range. The Navy desired a fighter with more performance than the F-4 Phantom II, yet in trials, the maneuverability and performance of the F-111B, especially in the crucial medium-altitude regimen, was decidedly inferior to the Phantom. During the congressional hearings for the aircraft, Vice Admiral Thomas "Tom Cat" Connolly, then CNO (Air), famously responded to a Senator's question as to whether a more powerful engine would cure the aircraft's woes, "There isn't enough power in all Christendom to make that airplane what we want!"

By October 1967, the Navy was finally convinced that the F-111B program was a lost cause and recommended its cancellation, which occurred in 1968 after seven had been delivered, two of which had crashed. The swing-wing configuration, TF-30 engines, Phoenix missiles and radar developed for this plane (and the earlier, cancelled F6D Missileer) were used on its replacement, the F-14 Tomcat, also designed by Grumman. The Tomcat would be large enough to carry the AWG-9 and Phoenix weapons system while exceeding the agility of the F-4 Phantom.

F-111C

The F-111C was an export version for Australia, combining F-111A/E avionics with the long-span wings and heavier landing gear originally designed for the F-111B. Twenty-four were originally ordered in 1963, although development delays and structural problems kept them from entering service until 1973.

Four aircraft were modified to RF-111C reconnaissance configuration, retaining their strike capability. The RF-111C carries a reconnaissance pack with four cameras and an infrared linescan unit.

F-111C aircraft have been equipped to carry Pave Tack FLIR/laser pods, and later underwent an extensive Avionics Upgrade Program, with AN/APQ-169 attack radar replacing the elderly AN/APQ-113, Texas Instruments AN/APQ-171 terrain-following radar, twin Honeywell H423 ring-laser gyro INS, GPS receiver, modern digital databus, mission computer, and stores-management system, and cockpit multi-function displays (MFDs). Their engines were updated to TF30-P-108/109RA standard, with 21,000 lbf (93 kN) thrust. Four ex-USAF F-111As were refitted to F-111C standard and delivered to Australia as attrition replacements.

In late 2001, wing fatigue problems were discovered with one of the F-111C fleet. As a result a decision was made in May 2002 to replace the wings with spares taken from ex-USAF F-111Fs stored at the Aerospace Maintenance and Regeneration Center. The short span wings underwent a refurbishment in Australia which included extending the span in effect making the wings the same as the F-111C and F-111G models.

F-111D

The F-111D was an upgraded F-111A equipped with newer Mark II avionics, more powerful engines, improved intake geometry, and an early "glass cockpit." First ordered in 1967, extensive development problems delayed service entry until 1974, and only 96 were built.

The F-111D used the new Triple Plow 2 intakes, which were located four inches (100 mm) further away from the airframe to prevent engine ingestion of the sluggish boundary layer air that was known to cause stalls in the TF30 turbofans. It had more powerful TF30-P-3 engines with 12,000 lbf (53 kN) dry and 18,500 lbf (82 kN) afterburning thrust.

More significant- and problematic- were the Mark II avionics. These were digitally integrated microprocessor systems, some of the first used by the USAF, offering tremendous capability, but substantial problems during introduction. The main radar was the General Electric AN/APQ-114, with Doppler beam-sharpening, moving target indicator (MTI), and continuous wave mode for guiding semi-active radar homing missiles (which the standard AN/APQ-113 set lacked). This was matched with an Autonetics inertial navigation /attack radar system, Marconi Doppler radar for navigation, a horizontal situation display, an IBM processor, and a Norden integrated systems display, with modern multi-function displays (MFDs). These last proved to be a major source of trouble, serving to multiply the development problems experienced with the individual systems. Considerable acrimony between the contractors resulted, and it took years before the problems were solved. F-111 crews considered the -D the most capable (and user-friendly) version of the aircraft when everything functioned, but that was rare before the 1980s. Incidentally, the F-111D was never equipped to carry what proved to be the 'Aardvark's' most useful sensor system, the AN/AVQ-26 Pave Tack pod.

The F-111D was withdrawn from service in 1992 for mothballing at AMARC.

F-111E

The F-111E was a simplified, interim model ordered after the prolonged teething troubles of the F-111D. It used the -D's Triple Plow 2 intakes and more powerful TF30-P-3 engines, but retained the -A's Mark I avionics.

Although conceived after the -D, the F-111E was actually delivered before it. The first flight of an -E was 20 August 1969. A total of 94 were built.

Some F-111Es were based at RAF Upper Heyford in Oxfordshire (United Kingdom) until 1993, and the type saw service in Operation Desert Storm. All F-111Es were withdrawn to storage in 1993 and 1994.

F-111F

The F-111F was the final F-111 variant produced for Tactical Air Command, with more modern and advanced Mark IIB avionics that were more capable than the F-111E and much more reliable than the F-111D. A total of 106 were produced between 1971 and 1976. The aircraft were initially assigned to the 366 TFW at Mountain Home AFB, Idaho. In 1978. the F-111Fs were reassigned to the 48 TFW based at RAF Lakenheath in the United Kingdom, with some assigned to the 57th Fighter Weapons Wing at Nellis AFB.

The F-111F's Mark IIB avionics suite used a simplified version of the FB-111A's radar, the AN/APQ-144, lacking some of the strategic bomber's operating modes but adding a new 2.5 mi (4.0 km) display ring. Although it was tested with digital moving-target indicator (MTI) capacity, it was not used in production sets. It used Texas Instruments AN/APQ-146 terrain-following radar, Litton inertial navigation, and the F-111E's Weapon Control Panel. The internal weapons bay was normally occupied by a AVQ-26 Pave Tack FLIR and laser designator system for the delivery of precision laser-guided munitions. The radar was subsequently upgraded to AN/APQ-161, with the AN/APQ-171 terrain-following set. The later Pacer Strike avionics update program added new digital electronics and databus.

The -F also used the Triple Plow 2 intakes, along with the substantially more powerful TF30-100 turbofan with 25,100 lbf (112 kN) afterburning thrust. This substantially improves the -F's performance, allowing a top speed of Mach 2.5 at altitude and enabling an unloaded F-111F to supercruise (fly at supersonic speeds without afterburner). In 1985-86, engines were upgraded to the TF30-P-111 turbofan.

The F-111F made its combat debut in Operation El Dorado Canyon against Libya in 1986, and performed superbly in Operation Desert Storm against Iraq, where it unexpectedly added the anti-armor ("tank-plinking ") role to its resume. In Desert Storm, F-111F completed 3.2 successful strike missions for every unsuccessful one, making it 47% more capable than the the next leading strike aircraft.

Various plans to upgrade the F-111F, including the adoption of the General Electric F110 engine (used in the F-14D Tomcat), were proposed, but not implemented because they might have interfered with the USAF's political efforts to build the F-22 Raptor. As a result, the last USAF F-111s were withdrawn from service on 27 July 1996, replaced by the F-15E Strike Eagle.

FB-111A/F-111G

The FB-111A was a strategic bomber version of the F-111 developed as an interim aircraft for the Strategic Air Command to replace the elegant but troublesome supersonic B-58 Hustler and early models of the B-52 Stratofortress. The planned replacement program, the Advanced Manned Strategic Aircraft, was proceeding slowly, and the Air Force was concerned that fatigue failures in the B-52 fleet would leave the strategic bomber fleet dangerously under strength. Although 263 planes were planned originally, the total was finally cut to just 76. The first production aircraft was delivered in 1968. The FB-111A never had an official popular name, but it was commonly called the "Switchblade."

The FB-111A was 2 ft 1.5 in (or 650 mm) longer than the F-111A, allowing carriage of about 585 gallons (or 2,214 L) extra fuel, and was fitted with the longer wings of the abortive F-111B and F-111K for greater range and load-carrying ability. A stronger undercarriage and landing gear compensated for the higher take-off weights (gross weight rose to 119,250 lb or 54,105 kg). All but the first aircraft had the Triple Plow 2 intakes and the TF30-P-7 with 12,500 lbf (or 56 kN) dry and 20,350 lbf (or 90 kN) afterburning thrust.

The FB-111A had new electronics, known as the SAC Mk IIB suite. The Mk IIB retained the F-111A's Texas Instruments AN/ANPQ-134 terrain-following radar and Honeywell AN/APN-167 radar altimeter. Radar was the General Electric AN/APQ-114, with a new north-oriented display, a beacon tracking mode, and a photo recording mode. To those components, the FB-111A added a Rockwell AN/AJN-16 inertial navigation system, Singer-Kearfott AN/APN-185 Doppler radar, and the Litton AN/ASQ-119 Astrotracker astrocompass, which allowed navigation by stellar positioning (a similar system had been used on the SR-71 Blackbird ). A Horizontal Situation Display was added along with the AN/AYK-6 cockpit display. A unique feature of the FB-111A was that the TFR was integrated into the automatic flight control system, allowing "hands-off" flight at high speeds and low levels (down to 200 feet), even in adverse weather.

Armament for the strategic bombing role was the Boeing AGM-69 SRAM (short-range attack missile) with had Mach 3 speed and 110 mile range. Two could be carried in the internal weapons bay and four more on the inner underwing pylons. Nuclear gravity bombs were also typical FB armament. Fuel tanks were often carried on the 3rd non-swivelling pylon of each wing. Promotional photos showed a conventional bombload to a theoretical total of 50, 750 lb (or 340 kg) M117 weapons on eight pylons and bomb bay, but it was never used in a conventional role. In 1990, the SRAM was withdrawn from service amid concerns about the integrity of its nuclear warhead in the case of fire, and subsequently only unpowered bombs were available.

The FB-111 became surplus to SAC's needs after the introduction of the Rockwell B-1B Lancer, and the remaining FB-111s were converted to a tactical configuration and renamed the F-111G. They were used primarily for training.

The F-111G did undergo an avionics upgrade program that added a digital computer, dual AN/ASN-41 ring-laser gyro INS, AN/APN-218 Doppler navigation, and an updated terrain-following radar. The astrocompass system was deleted.

The G model did not remain in USAF service for long, being mothballed in 1993, but 15 were bought by Australia to supplement its F-111Cs.

Several "stretched" FB-111 variants (the FB-111B, with F101 engines and a longer fuselage, and the greatly enlarged FB-111H, intended as a possible replacement for the B-1A after that project's cancellation) were proposed in the late 1970s, but none were ever built.

General Dynamics/Grumman EF-111A Raven

The General Dynamics/Grumman EF-111A Raven was an electronic warfare aircraft designed to replace the B-66 Destroyer in the United States Air Force. Its crews and maintainers often called it the "Spark-Vark", a play on the F-111's "Aardvark" nickname until 1996.

The USAF contracted with Grumman in 1974 to convert some existing General Dynamics F-111As into electronic warfare/electronic countermeasures (ECM) aircraft. The USAF had considered the Navy / Marine Corps Grumman EA-6B Prowler, but was reluctant to adopt a Navy aircraft. The EF-111 entered service in 1983 and served until it was retired in 1998. Afterwards, the Air Force began depending on Navy and Marine Corps EA-6Bs for electronic warfare support.

EF-111 design and development

In the late 1960s, the U.S. Air Force sought a replacement for aging EB-66 and EB-57 electronic warfare aircraft. The Air Force studied the use of Navy EA-6B Prowlers during 1967–68. However, the Air Force desired a penetrating electronic jamming aircraft with supersonic speed, and, in 1972, decided to modify F-111As into electronic warfare aircraft as a cost effective option.

In January 1974 the Air Force awarded electronic warfare study contracts to Grumman and General Dynamics. Grumman was selected as the EF-111 prime contractor in December 1974, then was awarded a contract to modify two F-111As into EF-111 prototypes in January 1975. The first fully equipped model, known then as the "Electric Fox", flew on 10 March 1977, and deliveries to combat units began in 1981. A total of 42 airframes were converted at a total cost of US$1.5 billion, the last delivered in 1985.

The Raven retained the F-111A's navigation systems, with a revised AN/APQ-160 radar primarily for ground mapping. The primary feature of the Raven, however, was the AN/ALQ-99E jamming system, developed from the Navy's ALQ-99 on the Prowler. The aircraft also utilized the ALR-62 Countermeasures Receiving System (CRS) as a Radar Homing and Warning (RHAW) System, the same system carried by all F-111 fighter/bomber models in the United States and Australia. The ALQ-99E primary electronics were installed in the weapons bay, with transmitters fitted in a 16 feet (4.9 m) long ventral "canoe" radome; the complete installation weighed some 6,000 pounds (2,700 kg). Receivers were installed in a fin-tip pod, or "football", similar to that of the EA-6B. The aircraft's electrical and cooling systems had to be extensively upgraded to support this equipment. The cockpit was also rearranged, with all flight and navigation displays relocated to the pilot's side, and flight controls except throttles being removed from the other seat, where the electronic warfare officer's instrumentation and controls were installed.

The EF-111 was unarmed. Its speed and acceleration were its main means of self-defense. It was not capable of firing anti-radiation missiles in the lethal SEAD role, which was a tactical limitation. The Raven's engines were upgraded to the more powerful TF30-P-9 of the D-model, with 12,000 pounds-force (53 kN) dry and 19,600 lbf (87 kN) afterburning thrust in 1986. From 1987 to 1994 the "Spark 'Vark" underwent an Avionics Modernization Program (AMP), similar to the Pacer Strike program for the F-model. This added a dual AN/ASN-41 ring laser gyroscope INS, AN/APN-218 Doppler radar, and an updated AN/APQ-146 terrain-following radar. Cockpit displays were upgraded with multi-function displays.

EF-111 operational history

The EF-111A achieved initial operational capability in 1983. The EF-111A received the official popular name Raven, although in service it acquired the nickname "Spark 'Vark". EF-111s first saw combat use with the 20th Tactical Fighter Wing at RAF Upper Heyford during Operation El Dorado Canyon against Libya in 1986, and Operation Just Cause in Panama during late 1989.

The Raven served in the Gulf War during Operation Desert Storm in 1991. On 17 January 1991, a USAF EF-111 crew of Captain James Denton and Captain Brent Brandon ("Brandini") achieved an unofficial kill against an Iraqi Dassault Mirage F1, which they managed to maneuver into the ground, making it the only member of the F-111/FB-111/EF-111 family to achieve an aerial victory over another aircraft.
No Coalition aircraft were lost to a radar-guided missile during Desert Storm while an EF-111 Raven was on station.

On 13 February 1991, EF-111A, AF Ser. No. 66-0023, callsign Ratchet 75, crashed into terrain while maneuvering to evade a perceived enemy aircraft threat killing the pilot, Capt Douglas L. Bradt, and the EWO, Capt Paul R. Eichenlaub. It was the only EF-111A lost during combat, the only loss killing its crew, and one of just three EF-111s lost in its history.

EF-111 - Later action

EF-111s were also deployed to Aviano Air Base, Italy in support of Operation Deliberate Force during the mid-1990s. The Raven also flew missions in Operation Provide Comfort, Operation Northern Watch and Operation Southern Watch.

The last deployment of the Raven was a detachment of EF-111s stationed at Al Kharj/Prince Sultan Air Base in Saudi Arabia until April 1998.

Shortly afterward, the USAF began withdrawing the final EF-111As from service, and placed them in storage at the Aerospace Maintenance and Regeneration Center (AMARC) at Davis-Monthan AFB, Arizona. The last EF-111s were retired on 2 May 1998, at Cannon AFB, New Mexico. These were the final USAF F-111s in service. EA-6B Prowlers took over the electronic warfare role for the U.S. Air Force, along with Navy and Marine Corps use.

F-111 foreign sales

Australia

The Australian government ordered 24 F-111 aircraft in 1963 to replace the RAAF 's English Electric Canberra in the bombing and tactical strike role. While the first aircraft was officially handed over in 1968, structural integrity problems found in the USAF fleet delayed the service entry of the F-111C until 1973, USAF F-4 Phantom IIs being leased as an interim measure. Four aircraft were modified to RF-111C reconnaissance configuration, retaining their strike capability.

A number of ex-USAF aircraft have been delivered to Australia, as attrition replacements and to enlarge the fleet. Four aircraft modified to F-111C status were delivered in 1982, while eighteen F-111G aircraft were purchased in 1992 and delivered in 1994. Additional stored USAF airframes are reserved as a spares source.

Since their introduction Australia's F-111s have been operated by No. 1 Squadron RAAF in the strike role with No. 6 Squadron RAAF operating the aircraft as an operational conversion unit. A temporary flight designated the Washington Flying Unit ferried Australia's first 12 aircraft from the United States in 1973 and F-111s have been loaned to the RAAF's Aircraft Research and Development Unit. While the F-111 has not seen combat in Australian service, it is known that F-111 aircraft were placed on high alert during the initial phase of the Australian-lead intervention (INTERFET ) into East Timor in 1999. During the first Gulf War in 1991, the United States Government asked Australia to deploy RF-111 aircraft to the Persian Gulf. This request was denied as the Australian government judged that these aircraft were too important to Australia's security to risk in a distant war.

The Royal Australian Air Force's F-111 fleet has at times been controversial. Controversies surrounding the F-111 include:

The long delay to the delivery of the aircraft was a significant political issue in the late 1960s and early 1970s. This occurred around the same time that massive delays and cost blowouts to the Sydney Opera House were making headlines, prompting some commentators to dub the F-111 the "Flying Opera House."

Their use by the Hawke federal government to take surveillance photos of the Franklin Dam project in Tasmania.

Poor work conditions for F-111 ground crew involved in sealing/de-sealing F-111 fuel tanks resulted in permanent brain damage to a number of ground crew before conditions were improved.

In Australian military and aviation circles, the F-111 Aardvark is affectionately known as the "Pig," because of its ability to hunt amongst the weeds like its namesake, referring to the F-111's Terrain Following ability, which was unique at the time of its introduction. Another, less generous explanation of the source of the nickname refers to the colloquialism "Pigs Might Fly." A third origin can be posited from the word Aardvark, which translates into English as "Earth Pig."

United Kingdom

The British government cancelled the BAC TSR.2 in 1965, citing the lower costs of the TFX and ordered 50 F-111K aircraft in 1967. The K would be an F-111A modified for British equipment and weapons eg the Martel anti-shipping missile and for a higher gross take off weight. Prototypes of both the strike and trainer aircraft were started and were in the final stages of build when the order was cancelled just over a year later. Updated estimates of performance indicated that range and speed at altitude would be worse than expected and fall short of the specification. Cost increase together with devaluation of the pound meant that the cost would be around £3 million each and this was the reason cited.As a substitute, Blackburn Buccaneers for the low level strike and F-4 Phantoms for RAF and FAA (naval) use were purchased instead.

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Source : Article General Dynamics F-111 Aardvark of Wikipedia ( authors )

Specifications (F-111F)

  • Crew : 2 (pilot and weapons system operator).
  • Length : 73.5 ft (22.4 m).
  • Height : 17.13 ft (or 5.22 m).
  • Wingspan spread : 63 ft (or 19.2 m).
  • Wingspan swept : 32 ft (or 9.74 m).
  • Wing area spread :657.4 ft² (or 61 m²).
  • Wing area Swept : 525 ft² (or 48.77 m²).
  • Empty weight : 47,480 lb (or 21,537 kg).
  • Loaded weight : 82,843 lb (or 37,577 kg).
  • Max. takeoff weight : 98,979 lb (or 44,896 kg).
  • Maximum speed : Mach 2.5 (or 1,650 mph, or 2,655 km/h).
  • Combat radius : 1,330 mi (or 1,160 nm, or 2,140 km).
  • Ferry range : 3,220 mi (or 2,800 nm, or 5,190 km).
  • Service ceiling : 56,650 ft (or 17,270 m).
  • Rate of climb : 25,890 ft/min (or 131.5 m/s).
  • Powerplant : Two Pratt & Whitney TF30-P-100 turbofans.
  • Dry thrust : 17,900 lbf (or 19.4 kN) each.
  • Thrust with afterburner : 25,100 lbf (or 112 kN) each.
  • Thrust/weight : 0.61.
  • Armament : One M61 Vulcan 20 mm gatling cannon. Bombs :31,500 lb (or 14,300 kg).

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Source : Article General Dynamics F-111 Aardvark of Wikipedia ( authors )
General Dynamics F-111 Aardvark - EF-111 Raven : Your comments on this subject
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