Boeing F/A-18E/F Super Hornet
|F/A-18E Super Hornet
F/A-18F Super Hornet
|A U.S. Navy F/A-18F Super Hornet conducts a mission over the Persian Gulf|
|Role||Carrier-based multirole fighter|
|National origin||United States|
Boeing Defense, Space & Security
|First flight||29 November 1995|
|Primary users||United States Navy
Royal Australian Air Force
|Number built||500 as of April 2011|
|Program cost||Total procurement: US$48.09 billion (through FY2011)|
|Developed from||McDonnell Douglas F/A-18 Hornet|
|Variants||Boeing EA-18G Growler|
The Boeing F/A-18E Super Hornet and related twin-seat F/A-18F are a twin-engine carrier-based multirole fighter aircraft variant based on the McDonnell Douglas F/A-18 Hornet. The F/A-18E single-seat and F/A-18F tandem-seat variants are larger and more advanced derivatives of the F/A-18C and D Hornet. The Super Hornet has an internal 20 mm M61 rotary cannon and can carry air-to-air missiles and air-to-surface weapons. Additional fuel can be carried in up to five external fuel tanks and the aircraft can be configured as an airborne tanker by adding an external air refueling system.
Designed and initially produced by McDonnell Douglas, the Super Hornet first flew in 1995. Full-rate production began in September 1997, after the merger of McDonnell Douglas and Boeing the previous month. The Super Hornet entered service with the United States Navy in 1999, replacing the Grumman F-14 Tomcat, which was retired in 2006, and serves alongside the original Hornet. The Royal Australian Air Force (RAAF), which has operated the F/A-18A as its main fighter since 1984, ordered the F/A-18F in 2007 to replace its aging F-111 fleet. RAAF Super Hornets entered service in December 2010.
- 1 Development
- 2 Design
- 3 Operational history
- 4 Variants
- 5 Operators
- 6 Specifications (F/A-18E/F)
- 7 Notable appearances in media
- 8 See also
- 9 References
- 10 External links
The Super Hornet is a further evolutionary redesign of the McDonnell Douglas F/A-18 Hornet, but the origins of the unique wing and tail configuration of the Super Hornet can be traced back to an internal Northrop project P-530, c. 1965. The design started as a substantial rework of the lightweight F-5E with a larger wing, twin tail fins and a distinctive leading edge root extension (LERX) which led to the "Cobra" nickname. It eventually flew as the Northrop YF-17 "Cobra" competing in the United States Air Force's Lightweight Fighter (LWF) program. The LWF aimed to produce a smaller and simpler fighter to complement the larger F-15 Eagle. The Navy directed that the YF-17 be redesigned into the larger F/A-18 Hornet which met a requirement for a smaller multi-role fighter to complement the larger F-14 Tomcat which served in air superiority and fleet defense interceptor roles. The Hornet proved to be effective and popular, but limited in combat radius. The ultimate evolution would grow the design into the Super Hornet with an empty weight slightly greater than the F-15C.
The concept of an enlarged Hornet was first proposed in 1980s, when an early version was marketed by McDonnell Douglas as Hornet 2000. The Hornet 2000 concept was an advanced version of the F/A-18 with a larger wing and a longer fuselage to carry more fuel and more powerful engines. The Hornet 2000 study was officially announced by McDonnell Douglas in January 1988. At the same time, U.S. Naval Aviation faced a number of problems. The McDonnell Douglas A-12 Avenger II program, intended to replace the obsolete Grumman A-6 Intruder and LTV A-7 Corsair II, had run into serious problems and was canceled. The end of the Cold War subsequently led to a period of military budget cuts and considerable restructuring.
With no clean-sheet program in the works, the Navy considered updating an existing design as a more attractive approach. As an alternative to the A-12, McDonnell Douglas proposed the "Super Hornet" (initially "Hornet II" in the 1980s), an improvement of the successful early F/A-18 models, which could serve as an alternate replacement for the A-6 Intruder. At the same time, the Navy needed a fleet defense fighter to replace the canceled Navy Advanced Tactical Fighter (NATF), which was to have developed a navalized variant of the Air Force's Lockheed Martin F-22 Raptor.
Testing and production
The Super Hornet was first ordered by the U.S. Navy in 1992. The Navy would also direct that this fighter replace the aging F-14 Tomcat, essentially basing all naval combat jets on Hornet variants until the introduction of the F-35C Lightning II. The Navy retained the F/A-18 designation to help sell the program to Congress as a low-risk "derivative", though the Super Hornet is largely a new aircraft. The Hornet and Super Hornet share many design and flight characteristics, including avionics, ejection seats, radar, armament, mission computer software, and maintenance/operating procedures. In particular the initial F/A-18E/F retained most of the avionics systems from the F/A-18C/D's configuration at the time.
The Super Hornet first flew on 29 November 1995. Initial production on the F/A-18E/F began in 1995. Flight testing started in 1996 with the F/A-18E/F's first carrier landing in 1997. Low-rate production began in March 1997 with full production beginning in September 1997. Testing continued through 1999, finishing with sea trials and aerial refueling demonstrations. Testing involved 3,100 test flights covering 4,600 flight hours. The Super Hornet underwent U.S. Navy operational tests and evaluations in 1999, and was approved in February 2000.
The Navy considers acquisition of the Super Hornet a success with it meeting cost, schedule, and weight (400 lb, 181 kg below) requirements. Despite having the same general layout and systems, the Super Hornet differs in many ways from the original F/A-18 Hornet. The Super Hornet is informally referred to as the "Rhino" to distinguish it from earlier model "legacy" Hornets and to prevent confusion in radio calls. This aids safe flight operations, since the catapult and arresting systems must be set differently for the heavier Super Hornet. (The "Rhino" nickname was earlier used by the McDonnell Douglas F-4 Phantom II, which was retired from the fleet in 1987.)
The U.S. Navy currently flies both the F/A-18E single-seater and F/A-18F two-seater in combat roles, taking the place of the retired F-14, A-6 Intruder, Lockheed S-3 Viking, and KA-6D. An electronic warfare variant, the EA-18G Growler, will replace the aging EA-6B Prowler. The Navy calls this reduction in aircraft types a "neck-down". In the Vietnam War era, the Super Hornet's capabilities were covered by no less than the A-1/A-4/A-7 (light attack), A-6 (medium attack), F-8/F-4 (fighter), RA-5C (recon), KA-3/KA-6 (tanker) and EA-6 (electronic warfare). It is anticipated that $1 billion in fleet wide annual savings will result from replacing other types with the Super Hornet.
In 2003, the Navy identified a flaw present in the under wing pylons across the Super Hornet fleet which required remedial repairs, or would otherwise decrease the aircraft's service life. As of 2007, changes to rectify the problem on newly manufactured airframes had been implemented, and existing aircraft would also receive modifications from 2009 onwards.
Improvements and changes
After initial fleet integration began, Boeing upgraded to the Block II version of the aircraft, incorporating an improved Active Electronically Scanned Array (AESA) radar, adopting larger displays, integrating the joint helmet mounted cuing system, and replacing many other avionics. The Block II configuration has the avionics and weapons systems that were being developed for the proposed production JSF version of the Boeing X-32. As part of the Block II configuration, new-build aircraft received the APG-79 AESA radar beginning in 2005; earlier production aircraft will have their APG-73 replaced with the APG-79. In January 2008, it was announced that 135 aircraft were to be retrofitted with AESA radars.
In early 2008, Boeing discussed the development of a Super Hornet Block III with the U.S. and Australian military, featuring additional stealth capabilities and extended range; a long-term successor is to be developed under the Next Generation Air Dominance program. In 2010, Boeing offered international customers the Super Hornet "International Roadmap", which included conformal fuel tanks, enhanced engines, an enclosed weapons pod (EWP), a next-generation cockpit, a new missile warning system, and an internal infra-red search and track (IRST) system. The enclosed weapons pods (EWP) are to have four internal stations for munitions; a total of three EWPs could be carried by a single aircraft, housing up to 12 AMRAAMs and 2 Sidewinders. The next-generation cockpit will feature a large 19 in x 11 inch touch-sensitive display.
In 2007, Boeing stated that a passive Infrared Search and Track (IRST) sensor would be a future option for the Super Hornet. The sensor, mounted in a modified centerline fuel tank, would detect long wave IR emissions for detecting and tracking targets such as other aircraft. The IRST coupled with the AIM-9X Block III Sidewinder missile will allow enemy aircraft to be engaged without disruption from radar jamming. On 18 May 2009, Lockheed Martin announced its selection by Boeing to conduct the IR sensor's technology development phase. Lockheed Martin was awarded a contract for the IRST in November 2011. As of September 2013[update], a basic IRST would be fielded in 2016 and a longer-range version in 2019; the 2013 sequestration cuts could delay those dates by two years.
In 2009, development had commenced on several engine improvements, including greater resistance to foreign object damage, reduced fuel burn rate, and potentially increased thrust of up to 20%. In late 2011, Boeing received a contract from the US Navy to develop a new mission computer for the Super Hornet.
Boeing and Northrop Grumman have been self-funding a prototype of the Advanced Super Hornet. The prototype features a 50% reduction in frontal radar cross-section (RCS), conformal fuel tanks (CFT), and an enclosed weapons pod. Features of the Advanced Super Hornet can also be integrated onto the EA-18G Growler; the adoption of CFTs on the EA-18 fleet has been speculated as useful to releasing underwing space and drag margin for the Next Generation Jammer. Flight tests of the Advanced Super Hornet began on 5 August 2013 and continued for three weeks, testing the performance of CFTs, the enclosed weapons pod (EWP), and signature enhancements.
In March 2013, the U.S. Navy was considering the widespread adoption of conformal fuel tanks, which would allow the Super Hornet to carry 3,500 lb (1,600 kg) of additional fuel. Budgetary pressures from the F-35C Lightning II and Pacific region operations were cited as reasons supporting the use of CFTs. Flight testing has demonstrated that the CFTs can slightly reduce drag, and the extra fuel expands the Super Hornet's combat radius by 260 nautical miles. While the prototype CFT weighs 1,500 lb, the production tank is expected to weigh only 870 lb. Boeing has stated that the CFTs do not add any cruise drag but acknowledge a negative impact imposed on transonic acceleration due to increased waved drag. General Electric's enhanced performance engine (EPE), increasing the power output of the F414-GE-400 from 22,000 lb to 26,400 lb of thrust per engine, has been suggested as a mitigating measure. The U.S. Navy is pleased with the results of flight tests of the Advanced Super Hornet configuration and hopes it will give lawmakers options when considering Super Hornet procurements in future budgets.
Boeing is considering a conceptual hybrid variant of the Super Hornet that would be equipped with electronic signal detection capabilities of the EA-18G Growler. The concept mainly relies on adding the Growler's ALQ-218 electronic receiver to the Super Hornet. With the Super Hornet carrying weapons that the Growler cannot, it would have the capability to engage targets it sees emitting signals by using the receiver; the concept does not include adding the ALQ-99 jamming pod. Growth capabilities could include the addition of a long-range infrared search and track sensor and new air-to-air tracking modes.
The Super Hornet is largely a new aircraft. It is about 20% larger, 7,000 lb (3,200 kg) heavier empty weight, and 15,000 lb (6,800 kg) heavier maximum weight than the original Hornet. The Super Hornet carries 33% more internal fuel, increasing mission range by 41% and endurance by 50% over the "Legacy" Hornet. The empty weight of the Super Hornet is about 11,000 lb (5,000 kg) less than that of the F-14 Tomcat which it replaced, while approaching, but not matching, the F-14's payload and range.[N 2]
The Super Hornet, unlike the previous Hornet, is designed so it can be equipped with an aerial refueling system (ARS) or "buddy store" for the refueling of other aircraft, filling the tactical airborne tanker role the Navy had lost with the retirement of the KA-6D and Lockheed S-3B Viking tankers. The ARS includes an external 330 US gal (1,200 L) tank with hose reel on the centerline, along with four external 480 US gal (1,800 L) tanks and internal tanks, for a total of 29,000 lb (13,000 kg) of fuel on the aircraft. On typical missions a fifth of the air wing is dedicated to the tanker role, which consumes aircraft fatigue life expectancy faster than other missions.
The forward fuselage is unchanged, but the remainder of the aircraft shares little with earlier F/A-18C/D models. The fuselage was stretched by 34 in (86 cm) to make room for fuel and future avionics upgrades and increased the wing area by 25%. However, the Super Hornet has 42% fewer structural parts than the original Hornet design. The General Electric F414 engine, developed from the Hornet's F404, has 35% additional thrust over most of the aircraft's flight envelope. The Super Hornet can return to an aircraft carrier with a larger load of unspent fuel and munitions than the original Hornet. The term for this ability is known as "bringback". Bringback for the Super Hornet is in excess of 9,000 lb (4,100 kg).
Other differences include approximately rectangular intakes for the engines and two extra wing hard points for payload (for a total of 11), retaining previous hardpoints on the bottom centerline, wingtips, and two conformal fuselage positions. Among the most significant aerodynamic changes are the enlarged leading edge extensions (LEX) which provide improved vortex lifting characteristics in high angle of attack maneuvers, and reduce the static stability margin to enhance pitching characteristics. This results in pitch rates in excess of 40 degrees per second, and high resistance to departure from controlled flight.
Radar signature reduction measures
Survivability is an important feature of the Super Hornet design. The U.S. Navy took a "balanced approach" to survivability in its design. This means that it does not rely on low-observable technology, such as stealth systems, to the exclusion of other survivability factors. Instead, its design incorporates a combination of stealth, advanced electronic-warfare capabilities, reduced ballistic vulnerability, the use of standoff weapons, and innovative tactics that cumulatively and collectively enhance the safety of the fighter and crew.
The F/A-18E/F's radar cross-section was reduced greatly from some aspects, mainly the front and rear. The design of the engine inlets reduces the aircraft's frontal radar cross-section. The alignment of the leading edges of the engine inlets is designed to scatter radiation to the sides. Fixed fanlike reflecting structures in the inlet tunnel divert radar energy away from the rotating fan blades.
The Super Hornet also makes considerable use of panel joint serration and edge alignment. Considerable attention has been paid to the removal or filling of unnecessary surface join gaps and resonant cavities. Where the F/A-18A-D used grilles to cover various accessory exhaust and inlet ducts, the F/A-18E/F uses perforated panels that appear opaque to radar waves at the frequencies used. Careful attention has been paid to the alignment of many panel boundaries and edges, to direct reflected waves away from the aircraft in uniformly narrow angles.
It is claimed that the Super Hornet employs the most extensive radar cross section reduction measures of any contemporary fighter, other than the F-22 and F-35. While the F/A-18E/F is not a true stealth fighter like the F-22, it will have a frontal radar cross-section an order of magnitude smaller than prior generation fighters. Additional RCS reduction measures can be installed on an as needed basis.
Initially, the Super Hornet's avionics and software had a 90% commonality with that of the F/A-18C/D fleet at the time. Differences include a touch-sensitive, up-front control display; a large liquid-crystal multipurpose color display; and a fuel display. The Super Hornet has a quadruplex digital fly-by-wire system, as well as a digital flight-control system that detects and corrects for battle damage. Initial production models used the APG-73 radar, later replaced by the APG-79 Active Electronically Scanned Array (AESA). The AN/ASQ-228 ATFLIR (Advanced Targeting Forward Looking InfraRed), is the main electro-optical sensor and laser designator pod for the Super Hornet. The communications equipment consist of an AN/ARC-210 VHF/UHF radio and a MIDS low volume terminal for HAVE QUICK, SINCGARS and Link 16 connectivity.
The defensive countermeasures of Block I aircraft includes the AN/ALR-67(V)3 radar warning receiver, the AN/ALE-47 countermeasures dispenser, the AN/ALE-50 towed decoy and the AN/ALQ-165 Airborne Self-Protect Jammer (ASPJ). Newer Block II aircraft replace the ALQ-165 with the AN/ALQ-214 Integrated Defensive Countermeasures (IDECM) system which consists of internally mounted threat receivers and optional self-protection jammers. The interior and exterior lighting on the Block II has also been changed to allow the air crew to use night vision goggles (NVG). The older ALE-50 decoys are being replaced by ALE-55 towed decoys, which can transmit jamming signals based on data received from the IDECM. The improved AN/ALQ-214 jammer was added on Super Hornet Block II.
The Super Hornet Block II configuration includes the new APG-79 AESA radar; it enables its crew to execute simultaneous air-to-air and air-to-ground attacks. The APG-79 also provides higher quality high-resolution ground mapping at long standoff ranges. The AESA radar can also detect smaller targets, such as inbound missiles and can track air targets beyond the range of the Super Hornet's own air to air missiles. VFA-213 became "safe for flight" (independently fly and maintain the F/A-18F) on 27 October 2006 and is the first Super Hornet squadron to fly AESA-equipped Super Hornets.
The first Super Hornet upgraded with the Joint Helmet Mounted Cueing System (JHMCS) was delivered to VFA-213 on 18 May 2007. The JHMCS provides multi-purpose situational awareness, which includes high-off-bore-sight missile cuing. The Shared Reconnaissance Pod (SHARP) is a high-resolution, digital tactical air reconnaissance system that features advanced day/night and all-weather capability. The Multifunctional Information Distribution System low volume communication terminal is being upgraded with the MIDS-JTRS system, which will allow a tenfold increase in bandwidth as well as compatibility with the Joint Tactical Radio System standards.
The Super Hornet achieved initial operating capability (IOC) in September 2001 with the U.S. Navy's Strike Fighter Squadron 115 (VFA-115) at Naval Air Station Lemoore, California. VFA-115 was also the first unit to take their F/A-18 Super Hornets into combat. On 6 November 2002, two F/A-18Es conducted a "Response Option" strike in support of Operation Southern Watch on two surface-to-air missile launchers at Al Kut, Iraq and an air defense command and control bunker at Tallil air base. One of the pilots, Lieutenant John Turner, dropped 2,000 lb (910 kg) JDAM bombs from the Super Hornet for the first time during combat.
In support of Operation Iraqi Freedom (Iraq War), VFA-14, VFA-41 and VFA-115 flew close air support, strike, escort, SEAD and aerial refueling sorties. Two F/A-18Es from VFA-14 and two F/A-18Fs from VFA-41 were forward deployed to the Abraham Lincoln. The VFA-14 aircraft flew mostly as aerial refuelers and the VFA-41 fighters as Forward Air Controller (Airborne) or FAC(A)s. On 6 April 2005, VFA-154 and VFA-147 (the latter squadron then still operating F/A-18Cs) dropped two 500-pound (230 kg) laser-guided bombs on an enemy insurgent location east of Baghdad.
On 8 September 2006, VFA-211 F/A-18F Super Hornets expended GBU-12 and GBU-38 bombs against Taliban fighters and Taliban fortifications west and northwest of Kandahar. This was the first time the unit was in combat with the Super Hornet.
During the 2006–2007 cruise with Dwight D. Eisenhower, VFA-103 and VFA-143 supported Operations Iraqi Freedom, Enduring Freedom and operations off the Somali coast. Alongside "Legacy Hornet" squadrons, VFA-131 and VFA-83, they dropped 140 precision guided weapons and performed nearly 70 strafing runs.
In 2007, Boeing proposed additional F/A-18E/Fs to the U.S. Navy in a multi-year contract. In 2008, it was reported that the Navy was considering buying additional F/A-18 Super Hornets to bridge a "strike-fighter" gap. As of October 2008, Boeing had delivered 367 Super Hornets to the U.S. Navy.
On 6 April 2009, Defense Secretary Gates announced that the Department of Defense intends to acquire further 31 F/A-18s in FY2010. Congressional action has requested that the DoD study a further multi-year contract in order to avoid a projected strike fighter shortfall. The FY2010 budget bill authorizes, but does not require, a multiyear purchase agreement for additional Super Hornets.
On 14 May 2010, it was reported that Boeing and the U.S. Department of Defense reached an agreement for a multi-year contract for an additional 66 F/A-18E/Fs and 58 EA-18Gs over the next four years. The latest order for 124 aircraft will raise the total fleet count to 515 F/A-18E/Fs and 114 EA-18Gs. However, the Navy is already 60 fighters below its validated requirement for fighter aircraft and this purchase will not close the gap. The deal was finalized on 28 September 2010 for a multi-year contract said to save $600 million (over per year contracts) for 66 Super Hornets and 58 Growlers and to help deal with a four-year delay in the F-35 Joint Strike Fighter program.
Royal Australian Air Force
On 3 May 2007, the Australian Government signed a contract to acquire 24 F/A-18Fs for the Royal Australian Air Force (RAAF), at a cost of A$2.9 billion, as an interim replacement for the aging F-111s. The total cost with training and support over 10 years is A$6 billion (US$4.6 billion).
The order was controversial, with critics including some retired senior RAAF officers. Air Vice Marshal (ret.) Peter Criss, a former Air Commander, said he was "absolutely astounded" that the Australian government would spend $6 billion on an interim aircraft. Criss has also cited evidence given by the U.S. Senate Armed Services Committee that the Super Hornet Block I specific excess power is inferior to the MiG-29 and Su-30, which have been operated, or ordered, by multiple air forces in South East Asia. Air Commodore (ret.) Ted Bushell stated that the F/A-18F could not perform the role that the Australian government had given it, and the F-111 would remain suitable for the strategic deterrent/strike role until at least 2020. Some critics have claimed that the decision to buy the F/A-18F could ease additional Super Hornet sales to Australia, particularly if the F-35 program "encounter more problems".
A review of the purchase was announced on 31 December 2007, by the new Australian Labor government, as part of a wider review of the RAAF's combat aircraft procurement plans. The main reasons given were concerns over operational suitability, the lack of a proper review process, and internal beliefs that an interim fighter was not required. On 17 March 2008, the Government announced that it would proceed with plans to acquire all 24 F/A-18Fs. Defence Minister Joel Fitzgibbon said that the Super Hornet was an "excellent aircraft". However, Fitzgibbon also indicated that costs and logistical factors contributed to the decision: the F-111's retirement was "irreversible"; the F/A-18F was "the only aircraft" that could "meet the small delivery window", and "cancelling the Super Hornet would bring significant financial penalties and create understandable tensions between the contract partners."
The Block II package aircraft offered to the RAAF include installed engines and six spares, APG-79 AESA radars, Link 16 connectivity, LAU-127 guided missile launchers, AN/ALE-55 fiber optic towed decoys and other equipment. The government has also sought U.S. export approval for Boeing EA-18G Growlers. On 27 February 2009, Fitzgibbon announced that 12 of the 24 Super Hornets would be wired on the production line for future modification as EA-18Gs. The additional wiring would cost A$35 million. The final decision on conversion to EA-18Gs, at a cost of A$300 million, would be made in 2012.
The first RAAF Super Hornet was completed in 2009 and first flew from Boeing's factory in St. Louis, Missouri on 21 July 2009. RAAF pilots and air combat officers began training in the USA in 2009, with No. 1 Squadron planned to become fully operational with the F/A-18F in 2010. The RAAF's first five Super Hornets arrived at their home base, RAAF Base Amberley in Queensland, on 26 March 2010. These initial aircraft were joined by six more aircraft on 7 July 2010. With the arrival of another four aircraft in December 2010, the first RAAF F/A-18F squadron was declared operational on 9 December 2010.
In December 2012, the Australian government sought information from the United States government about the cost of acquiring a further 24 F/A-18Fs. These aircraft may be purchased to avoid a capability gap developing due to delays to the F-35 program. In February 2013, the U.S. Defense Security Cooperation Agency notified Congress of a possible Foreign Military Sale to Australia for up to 12 F/A-18E/F Super Hornet and 12 EA-18G Growler aircraft with associated equipment, parts, training and logistical support. In May 2013, Australia announced they would keep the 24 F/A-18F Super Hornets they currently have instead of converting them, and will order 12 new-built EA-18G Growlers. The government remains committed to the F-35 Lightning II acquisition.
The United States Marine Corps has avoided the Super Hornet program and their resistance is so high that they would rather fly former Navy F/A-18Cs that have been replaced with Super Hornets. This is said to be because they fear that any Super Hornet buys will be at the cost of the F-35B STOVL fighters that they intend to operate from amphibious ships. As a concession, the Marine Corps has agreed to eventually equip five Marine fighter-attack squadrons (VMFA) with the F-35C carrier variant to continue to augment Navy carrier air wings as they currently do with the F/A-18C.
Boeing offered Malaysia the Super Hornets as part of a buy-back package for its existing F/A-18 Hornets in 2002. However, the Super Hornet procurement was halted in 2007 after the government decided to purchase the Sukhoi Su-30MKM instead. But RMAF Chief Gen. Datuk Nik Ismail Nik Mohamaed indicated that the RMAF had not planned to end procurement of the Super Hornets, instead saying that the air force needed such fighters.
Boeing proposed the Super Hornet to the Brazilian government. It was reported that the Super Hornet was selected as one of three finalists in Brazil's fighter competition in October 2008. Brazil has put forward an initial requirement for 36 aircraft, with a potential total purchase of 120 examples. However news of NSA's spying activity on Brazilian leaders has caused animosity between Brazil and the US. Brazil eventually dropped the Super Hornet from its final list and selected the Saab JAS 39 Gripen in December 2013.
In 2008, the Royal Danish Air Force was offered the Super Hornet. The Super Hornet is one of three fighter aircraft in a Danish competition to replace 48 F-16AM/BMs. The other contenders are Lockheed Martin's F-35A Joint Strike Fighter and the Eurofighter Typhoon. Denmark is a level-3 partner in the JSF program, and has invested US$200 million so far. The final selection is to be in mid-2015 where 24 to 30 fighters are expected. In April 2014, the Danish Ministry of Defence handed over a Request for Binding Information (RBI) that specifically listed the F/A-18F two-seat variant.
For India's MMRCA competition, Boeing offered a customized variant called F/A-18IN, which included Raytheon's APG-79 AESA radar. In August 2008, Boeing submitted an industrial participation proposal to India describing partnerships with companies in India. The Indian Air Force (IAF) extensively evaluated the Super Hornets and conducted field trials in August 2009. However, in April 2011, the IAF rejected F/A-18IN's bid in favor of the Eurofighter Typhoon and Dassault Rafale.
On 10 March 2009, Boeing offered the Super Hornet for Greece's Next-Generation Fighter Program.
On 1 August 2010, The Sunday Times reported that the British government was considering canceling orders for the Lockheed Martin F-35 Lightning II and buying the Super Hornet instead for its Queen Elizabeth class aircraft carriers. It was stated that this would save the UK defense budget about £10 billion. An industry source suggested that the Super Hornet could be ski jump launched without catapults. The UK has reverted to a STOVL aircraft carrier equipped with F-35B fighters.
The United Arab Emirates has asked for information on the Super Hornet.
Boeing stated that the "stealth characteristics" of the Super Hornet were ignored in Canada's sole source selection of the F-35. In April 2012, Canada was reviewing its plans to procure the F-35 and may consider buying the Super Hornet instead. In September 2013, Boeing provided Canada with cost and capability data for its Advanced F/A-18 Super Hornet, suggesting that a fleet of 65 aircraft would cost $1.7 billion less than a fleet of F-35s. The Advanced Super Hornet builds upon the existing Super Hornet, which is an improvement of the current CF-18 Hornet. The U.S. Navy buys Super Hornets for $52 million per aircraft, while the advanced version would add $6–$10 million per aircraft, depending on options selected.
In early 2011, Bulgaria was considering the F/A-18 Super Hornet, among other aircraft, as a replacement for its MiG-21 fleet.
On 12 March 2014, Belgian Newspaper "De Morgen" reported that Boeing is in talks with the Belgian Defence ministry about the Super Hornet as a candidate to replace Belgium's aging F-16 fleet.
Poland is planning to purchase 64 multirole combat aircraft from 2021 as part of that country's modernization plans. The new fighters will replace the Polish Air Force's fleet of Sukhoi Su-22M4 ground attack aircraft and Mikoyan MiG-29 fighter aircraft. The planned open tender procedure could include the F-35 Lightning II, JAS 39 Gripen E/F, the newest variants of Eurofighter Typhoon and Dassault Rafale, and Boeing's F/A-18E/F Advanced Super Hornet.
- F/A-18E Super Hornet: single seat variant.
- F/A-18F Super Hornet: two-seat variant.
- EA-18G Growler: The electronic warfare version of the F/A-18F Super Hornet. Went into low rate production in 2007, with fleet deployment in 2009. The EA-18G will replace the U.S. Navy's Northrop Grumman EA-6B Prowler.
- United States Navy
- Pacific Fleet
- VFA-2 "Bounty Hunters" (F/A-18F)
- VFA-14 "Tophatters" (F/A-18E)
- VFA-22 "Fighting Redcocks" (F/A-18F)
- VFA-25 "Fist of the Fleet" (F/A-18E)
- VFA-27 "Royal Maces" (F/A-18E)
- VFA-41 "Black Aces" (F/A-18F)
- VFA-86 "Sidewinders" (F/A-18E)
- VFA-97 "Warhawks" (F/A-18E)
- VFA-102 "Diamondbacks" (F/A-18F)
- VFA-115 "Eagles" (F/A-18E)
- VFA-122 "Flying Eagles" (Fleet Replacement Squadron, operates F/A-18E/F)
- VFA-137 "Kestrels" (F/A-18E/F)
- VFA-147 "Argonauts" (F/A-18E)
- VFA-151 "Vigilantes" (F/A-18E)
- VFA-154 "Black Knights" (F/A-18F)
- VFA-195 "Dambusters" (F/A-18E)
- Atlantic Fleet
- VFA-11 "Red Rippers" (F/A-18F)
- VFA-31 "Tomcatters" (F/A-18E)
- VFA-32 "Swordsmen" (F/A-18F)
- VFA-34 "Blue Blasters" (F/A-18E) *Starting transition in Late 2012
- VFA-81 "Sunliners" (F/A-18E)
- VFA-103 "Jolly Rogers" (F/A-18F)
- VFA-105 "Gunslingers" (F/A-18E)
- VFA-106 "Gladiators" (Fleet Replacement Squadron, operates F/A-18A/B/C/D/E/F)
- VFA-136 "Knighthawks" (F/A-18E)
- VFA-143 "Pukin' Dogs" (F/A-18E)
- VFA-211 "Fighting Checkmates" (F/A-18F)
- VFA-213 "Black Lions" (F/A-18F)
- Test and Evaluation Units
- VX-9 Vampires (Air Test and Evaluation Squadron, operates F/A-18E/F and other aircraft)
- VX-23 Salty Dogs (Air Test and Evaluation Squadron, operates F/A-18E/F and other aircraft)
- VX-31 Dust Devils (Air Test and Evaluation Squadron, operates F/A-18E/F and other aircraft)
- NSAWC (Naval Strike and Air Warfare Center), F/A-18F, also operates other aircraft)
- Future F/A-18E/F squadrons (All to be Pacific Fleet squadrons)
- Pacific Fleet
Each United States Navy squadron has a standard unit establishment of 10 or 12 aircraft.
- Crew: F/A-18E: 1, F/A-18F: 2
- Length: 60 ft 1¼ in (18.31 m)
- Wingspan: 44 ft 8½ in (13.62 m)
- Height: 16 ft (4.88 m)
- Wing area: 500 ft² (46.5 m²)
- Empty weight: 32,081 lb (14,552 kg)
- Loaded weight: 47,000 lb (21,320 kg) (in fighter configuration))
- Max. takeoff weight: 66,000 lb (29,937 kg)
- Powerplant: 2 × General Electric F414-GE-400 turbofans
- Dry thrust: 13,000 lbf (62.3 kN) each
- Thrust with afterburner: 22,000 lbf (97.9 kN) each
- Internal fuel capacity: F/A-18E: 14,400 lb (6,780 kg), F/A-18F: 13,550 lb (6,354 kg)
- External fuel capacity: 5 × 480 gal tanks, totaling 16,380 lb (7,381 kg)
- Maximum speed: Mach 1.8 (1,190 mph, 1,915 km/h) at 40,000 ft (12,190 m)
- Range: 1,275 nmi (2,346 km) clean plus two AIM-9s
- Combat radius: 390 nmi (449 mi, 722 km) for interdiction mission
- Ferry range: 1,800 nmi (2,070 mi, 3,330 km)
- Service ceiling: 50,000+ ft (15,000+ m)
- Rate of climb: 44,882 ft/min (228 m/s)
- Wing loading: 94.0 lb/ft² (459 kg/m²)
- Thrust/weight: 0.93
- Design load factor: 7.6 g
- Guns: 1× 20 mm (0.787 in) M61A2 Vulcan nose-mounted Gatling-style cannon, 578 rounds
- Hardpoints: 11 total: 2× wingtips, 6× under-wing, and 3× under-fuselage with a capacity of 17,750 lb (8,050 kg) external fuel and ordnance
- Missiles: **Air-to-air missiles:
- Air-to-surface missiles:
- AGM-65 Maverick
- AGM-84H/K Standoff Land Attack Missile Expanded Range (SLAM-ER)
- AGM-88 HARM Anti-radiation missile
- AGM-154 Joint Standoff Weapon (JSOW)
- AGM-158 Joint Air-to-Surface Standoff Missile (JASSM)
- Anti-ship missile:
- Bombs: **JDAM precision-guided munition (PGMs)
- SUU-42A/A Flares/Infrared decoys dispenser pod and chaff pod or
- Electronic countermeasures (ECM) pod or
- AN/ASQ-228 ATFLIR Targeting pods or
- up to 3× 330 U.S. gallon (1,200 L) Sargent Fletcher drop tanks for ferry flight or extended range/loitering time or
- 1× 330 U.S. gal (1,200 L) tank and 4× 480 U.S. gal (1,800 L) tanks for aerial refueling system (ARS).
- Hughes APG-73 or Raytheon APG-79 Radar
- Northrop Grumman/ITT AN/ALE-165 self-protection jammer pod or BAE Systems AN/ALE-214 integrated defensive electronic countermeasures system
- Raytheon AN/ALE-50 or BAE Systems AN/ALE-55 towed decoy
- Northrop Grumman AN/ALR-67(V)3 radar warning receiver
- MIDS LVT or MIDS JTRS datalink transceiver
Notable appearances in media
- Related development
- Aircraft of comparable role, configuration and era
- Dassault Rafale
- Eurofighter Typhoon
- Grumman F-14 Tomcat
- McDonnell Douglas F-15E Strike Eagle
- Mikoyan MiG-29K
- Saab JAS 39 Gripen (Gripen NG)
- Sukhoi Su-33
- Related lists
- List of fighter aircraft
- List of active United States military aircraft
- List of United States military aerial refueling aircraft
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|Wikimedia Commons has media related to F/A-18E/F Super Hornet.|
- F/A-18 U.S. Navy fact file, and F/A-18 Navy history page
- F/A-18E/F Super Hornet page and F/A-18 Schematics on GlobalSecurity.org
- "USS Enterprise aircraft deliver lethal sting of bombs to enemy in Afghanistan", Stars and Stripes, 13 October 2006.
- Operational Lessons Learned from the F/A-18E/F Total Flight. Control Systems Integration Process.