General Dynamics F-16 Fighting Falcon
The Fighting Falcon's key features include a frameless bubble canopy
for better visibility, side-mounted control stick
to ease control while maneuvering, an ejection seat reclined 30 degrees from vertical to reduce the effect of g-forces
on the pilot
, and the first use of a relaxed static stability
flight control system that helps to make it an agile
aircraft. The F-16 has an internal M61 Vulcan
cannon and 11 locations for mounting weapons and other mission equipment. The F-16's official name is "Fighting Falcon", but "Viper" is commonly used by its pilots and crews, due to a perceived resemblance to a viper
snake as well as the Colonial Viper starfighter
on Battlestar Galactica
which aired at the time the F-16 entered service.
Lightweight Fighter program
Air Force F-X proponents remained hostile to the concept because they perceived it as a threat to the F-15
program, but the USAF's leadership understood that its budget would not allow it to purchase enough F-15 aircraft to satisfy all of its missions.
The Advanced Day Fighter concept, renamed F-XX
, gained civilian political support under the reform-minded Deputy Secretary of Defense David Packard
, who favored the idea of competitive prototyping
. As a result, in May 1971, the Air Force Prototype Study Group was established, with Boyd a key member, and two of its six proposals would be funded, one being the Lightweight Fighter
(LWF). The request for proposals
issued on 6 January 1972 called for a 20,000-pound (9,100 kg) class air-to-air day fighter with a good turn rate, acceleration, and range, and optimized for combat at speeds of Mach 0.6–1.6 and altitudes of 30,000–40,000 feet (9,100–12,000 m). This was the region where USAF studies predicted most future air combat would occur. The anticipated average flyaway cost of a production version was $3 million. This production plan, though, was only notional, as the USAF had no firm plans to procure the winner.
Selection of finalists and flyoff
A right-side view of a YF-16 (foreground) and a Northrop YF-17
, each armed with AIM-9 Sidewinder missiles
Five companies responded, and in 1972, the Air Staff selected General Dynamics' Model 401 and Northrop's P-600 for the follow-on prototype development and testing phase. GD and Northrop were awarded contracts worth $37.9 million and $39.8 million to produce the YF-16 and YF-17
, respectively, with the first flights of both prototypes planned for early 1974. To overcome resistance in the Air Force hierarchy, the Fighter Mafia
and other LWF proponents successfully advocated the idea of complementary fighters in a high-cost/low-cost force mix. The "high/low mix" would allow the USAF to be able to afford sufficient fighters for its overall fighter force structure requirements. The mix gained broad acceptance by the time of the prototypes' flyoff, defining the relationship of the LWF and the F-15.
The YF-16 was developed by a team of General Dynamics engineers led by Robert H. Widmer
The first YF-16 was rolled out on 13 December 1973. Its 90-minute maiden flight
was made at the Air Force Flight Test Center at Edwards AFB
, California, on 2 February 1974. Its actual first flight occurred accidentally during a high-speed taxi test on 20 January 1974. While gathering speed, a roll-control oscillation caused a fin of the port-side wingtip-mounted missile and then the starboard stabilator
to scrape the ground, and the aircraft then began to veer off the runway. The test pilot, Phil Oestricher, decided to lift off to avoid a potential crash, safely landing six minutes later. The slight damage was quickly repaired and the official first flight occurred on time. The YF-16's first supersonic flight was accomplished on 5 February 1974, and the second YF-16 prototype first flew on 9 May 1974. This was followed by the first flights of Northrop's YF-17 prototypes on 9 June and 21 August 1974, respectively. During the fly off, the YF-16s completed 330 sorties
for a total of 417 flight hours;
the YF-17s flew 288 sorties, covering 345 hours.
Air Combat Fighter competition
Increased interest turned the LWF into a serious acquisition program. North Atlantic Treaty Organization
(NATO) allies Belgium
, the Netherlands
, and Norway
were seeking to replace their F-104G Starfighter fighter-bombers
In early 1974, they reached an agreement with the U.S. that if the USAF ordered the LWF winner, they would consider ordering it as well. The USAF also needed to replace its F-105 Thunderchief
and F-4 Phantom II
fighter-bombers. The U.S. Congress sought greater commonality in fighter procurements by the Air Force and Navy, and in August 1974 redirected Navy funds to a new Navy Air Combat Fighter program that would be a navalized fighter-bomber variant of the LWF. The four NATO allies had formed the Multinational Fighter Program Group (MFPG) and pressed for a U.S. decision by December 1974; thus, the USAF accelerated testing.
To reflect this serious intent to procure a new fighter-bomber, the LWF program was rolled into a new Air Combat Fighter (ACF) competition in an announcement by U.S. Secretary of DefenseJames R. Schlesinger
in April 1974. The ACF would not be a pure fighter, but multi-role
, and Schlesinger made it clear that any ACF order would be in addition to the F-15, which extinguished opposition to the LWF.
ACF also raised the stakes for GD and Northrop because it brought in competitors intent on securing what was touted at the time as "the arms deal of the century".
These were Dassault-Breguet's
proposed Mirage F1M-53
, the Anglo-French SEPECAT Jaguar
, and the proposed Saab 37E "Eurofighter"
. Northrop offered the P-530 Cobra, which was similar to the YF-17. The Jaguar and Cobra were dropped by the MFPG early on, leaving two European and the two U.S. candidates. On 11 September 1974, the U.S. Air Force confirmed plans to order the winning ACF design to equip five tactical fighter wings. Though computer modeling predicted a close contest, the YF-16 proved significantly quicker going from one maneuver to the next and was the unanimous choice of those pilots that flew both aircraft.
On 13 January 1975, Secretary of the Air ForceJohn L. McLucas
announced the YF-16 as the winner of the ACF competition.
The chief reasons given by the secretary were the YF-16's lower operating costs, greater range, and maneuver performance that was "significantly better" than that of the YF-17, especially at supersonic speeds. Another advantage of the YF-16 – unlike the YF-17 – was its use of the Pratt & Whitney F100
turbofan engine, the same powerplant
used by the F-15; such commonality would lower the cost of engines for both programs.
Secretary McLucas announced that the USAF planned to order at least 650, possibly up to 1,400 production F-16s. In the Navy Air Combat Fighter competition, on 2 May 1975 the Navy selected the YF-17 as the basis for what would become the McDonnell Douglas F/A-18 Hornet
Commencement of production
The U.S. Air Force initially ordered 15 full-scale development (FSD) aircraft (11 single-seat and four two-seat models) for its flight test program, but was reduced to eight (six F-16A single-seaters and two F-16B two-seaters).
The YF-16 design was altered for the production F-16. The fuselage was lengthened by 10.6 in (0.269 m), a larger nose radome was fitted for the AN/APG-66
radar, wing area was increased from 280 sq ft (26 m2
) to 300 sq ft (28 m2
), the tailfin height was decreased, the ventral fins were enlarged, two more stores stations were added, and a single door replaced the original nosewheel double doors. The F-16's weight was increased by 25% over the YF-16 by these modifications.
The FSD F-16s were manufactured by General Dynamics in Fort Worth, Texas
at United States Air Force Plant 4
in late 1975; the first F-16A rolled out on 20 October 1976 and first flew on 8 December. The initial two-seat model achieved its first flight on 8 August 1977. The initial production-standard F-16A flew for the first time on 7 August 1978 and its delivery was accepted by the USAF on 6 January 1979. The F-16 was given its name of "Fighting Falcon" on 21 July 1980, entering USAF operational service with the 34th Tactical Fighter Squadron
, 388th Tactical Fighter Wing
at Hill AFB
in Utah on 1 October 1980.
On 7 June 1975, the four European partners, now known as the European Participation Group
, signed up for 348 aircraft at the Paris Air Show
. This was split among the European Participation Air Forces (EPAF) as 116 for Belgium, 58 for Denmark, 102 for the Netherlands, and 72 for Norway. Two European production lines, one in the Netherlands at Fokker
's Schiphol-Oost facility and the other at SABCA's Gosselies
plant in Belgium, would produce 184 and 164 units respectively. Norway's Kongsberg Vaapenfabrikk
and Denmark's Terma A/S
also manufactured parts and subassemblies for EPAF aircraft. European co-production was officially launched on 1 July 1977 at the Fokker factory. Beginning in November 1977, Fokker-produced components were sent to Fort Worth for fuselage assembly, then shipped back to Europe for final assembly of EPAF aircraft at the Belgian plant on 15 February 1978; deliveries to the Belgian Air Force
began in January 1979. The first Royal Netherlands Air Force
aircraft was delivered in June 1979. In 1980, the first aircraft were delivered to the Royal Norwegian Air Force
by SABCA and to the Royal Danish Air Force
During the late 1980s and 1990s, Turkish Aerospace Industries
(TAI) produced 232 Block
30/40/50 F-16s on a production line in Ankara under license
for the Turkish Air Force
. TAI also produced 46 Block 40s for Egypt in the mid-1990s and 30 Block 50 from 2010. Korean Aerospace Industries
opened a production line for the KF-16 program, producing 140 Block 52s from the mid-1990s to mid-2000s (decade). If India had selected the F-16IN for its Medium Multi-Role Combat Aircraft
procurement, a sixth F-16 production line would have been built in India.
In May 2013, Lockheed Martin stated there were currently enough orders to keep producing the F-16 until 2017.
Improvements and upgrades
One change made during production was augmented pitch control to avoid deep stall
conditions at high angles of attack. The stall issue had been raised during development but had originally been discounted. Model tests of the YF-16 conducted by the Langley Research Center
revealed a potential problem, but no other laboratory was able to duplicate it. YF-16 flight tests were not sufficient to expose the issue; later flight testing on the FSD aircraft demonstrated a real concern. In response, the area of each horizontal stabilizer was increased by 25% on the Block 15 aircraft in 1981 and later retrofitted to earlier aircraft. In addition, a manual override switch to disable the horizontal stabilizer flight limiter was prominently placed on the control console, allowing the pilot to regain control of the horizontal stabilizers (which the flight limiters otherwise lock in place) and recover. Besides reducing the risk of deep stalls, the larger horizontal tail also improved stability and permitted faster takeoff rotation.
In the 1980s, the Multinational Staged Improvement Program (MSIP) was conducted to evolve the F-16's capabilities, mitigate risks during technology development, and ensure the aircraft's worth. The program upgraded the F-16 in three stages. The MSIP process permitted the quick introduction of new capabilities, at lower costs and with reduced risks compared to traditional independent upgrade programs.
In 2012, the USAF had allocated $2.8 billion to upgrade 350 F-16s while waiting for the F-35 to enter service.
One key upgrade has been an auto-GCAS (Ground collision avoidance system
) to reduce instances of controlled flight into terrain
Onboard power and cooling capacities limit the scope of upgrades, which often involve the addition of more power-hungry avionics.
Lockheed won many contracts to upgrade foreign operators' F-16s. BAE Systems also offers various F-16 upgrades, receiving orders from South Korea, Oman, Turkey, and the US Air National Guard;
BAE lost the South Korean contract due to a price breach in November 2014.
In 2012, the USAF assigned the total upgrade contract to Lockheed Martin.
Upgrades include Raytheon's Center Display Unit, which replaces several analog flight instruments with a single digital display.
In 2013, sequestration budget cuts
cast doubt on the USAF's ability to complete the Combat Avionics Programmed Extension Suite (CAPES), a part of secondary programs such as Taiwan's F-16 upgrade. Air Combat Command
's General Mike Hostage
stated that if he only had money for a service life extension program (SLEP) or CAPES, he would fund SLEP to keep the aircraft flying.
Lockheed Martin responded to talk of CAPES cancellation with a fixed-price upgrade package for foreign users.
CAPES was not included in the Pentagon's 2015 budget request.
The USAF said that the upgrade package will still be offered to the Republic of China Air Force
, and Lockheed said that some common elements with the F-35 will keep the radar's unit costs down.
In 2014, the USAF issued a RFI to SLEP 300 F-16 C/Ds.
To make more room for assembly of its newer F-35 Lightning II
fighter aircraft, Lockheed Martin moved the F-16 production from Fort Worth, Texas to its plant in Greenville, South Carolina
Lockheed delivered the last F-16 from Fort Worth to the Iraqi Air Force
on 14 November 2017, ending 40 years of F-16 production there. The company is hoping to finish the Greenville move and restart production in 2019, though engineering and modernization work will remain in Fort Worth.
A gap in orders made it possible to stop production during the move; after completing orders for the last Iraqi purchase,
the company was negotiating an F-16 sale to Bahrain
that would be produced in Greenville. This contract was signed in June 2018.
Comparison between F-16's inset cannon; early aircraft had four leading vents, a grille, and four trailing vents, while later aircraft had two trailing vents only.
The F-16 is a single-engine, highly maneuverable, supersonic, multi-role tactical fighter aircraft. It is much smaller and lighter than its predecessors but uses advanced aerodynamics
and avionics, including the first use of a relaxed static stability
(RSS/FBW) flight control system, to achieve enhanced maneuver performance. Highly agile, the F-16 was the first fighter aircraft purpose-built to pull 9-g
maneuvers and can reach a maximum speed of over Mach
2. Innovations include a frameless bubble canopy for better visibility, a side-mounted control stick, and a reclined seat to reduce g-force
effects on the pilot. It is armed with an internal M61 Vulcan cannon
in the left wing root and has multiple locations for mounting various missiles, bombs and pods. It has a thrust-to-weight ratio greater than one, providing power to climb and vertical acceleration.
The F-16 was designed to be relatively inexpensive to build and simpler to maintain than earlier-generation fighters. The airframe is built with about 80% aviation-grade aluminum alloys
, 8% steel, 3% composites, and 1.5% titanium
. The leading-edge flaps, stabilators
, and ventral fins make use of bonded aluminum honeycomb structures
and graphite epoxy laminationcoatings
. The number of lubrication points, fuel line connections, and replaceable modules
is significantly lower than preceding fighters; 80% of the access panels can be accessed without stands.
The air intake was placed so it was rearward of the nose but forward enough to minimize air flow losses and reduce aerodynamic drag
Although the LWF program called for a structural life of 4,000 flight hours, capable of achieving 7.33 g
with 80% internal fuel; GD's engineers decided to design the F-16's airframe life for 8,000 hours and for 9-g
maneuvers on full internal fuel. This proved advantageous when the aircraft's mission changed from solely air-to-air combat to multi-role operations. Changes in operational use and additional systems have increased weight, necessitating multiple structural strengthening programs.
The F-16 has a cropped-delta wing
incorporating wing-fuselage blending
and forebody vortex
; a fixed-geometry, underslung air intake (with splitter plate
) to the single turbofan jet engine; a conventional tri-plane empennage
arrangement with all-moving horizontal "stabilator
" tailplanes; a pair of ventral fins beneath the fuselage aft of the wing's trailing edge; and a tricycle landing gear
configuration with the aft-retracting, steerable nose gear deploying a short distance behind the inlet lip. There is a boom-style aerial refueling
receptacle located behind the single-piece "bubble" canopy of the cockpit. Split-flap speedbrakes
are located at the aft end of the wing-body fairing, and a tailhook
is mounted underneath the fuselage. A fairing beneath the rudder often houses ECM equipment or a drag chute
. Later F-16 models feature a long dorsal fairing along the fuselage's "spine", housing additional equipment or fuel.
Aerodynamic studies in the 1960s demonstrated that the "vortex lift
" phenomenon could be harnessed by highly swept wing
configurations to reach higher angles of attack
, using leading edge
vortex flow off a slender lifting surface. As the F-16 was being optimized for high combat agility, GD's designers chose a slender cropped-delta wing with a leading-edge sweep of 40° and a straight trailing edge. To improve maneuverability, a variable-camber
wing with a NACA 64A-204 airfoil
was selected; the camber is adjusted by leading-edge and trailing edge flaperons
linked to a digital flight control system
regulating the flight envelope
The F-16 has a moderate wing loading, reduced by fuselage lift.
The vortex lift effect is increased by leading-edge extensions, known as strakes. Strakes act as additional short-span, triangular wings running from the wing root
(the junction with fuselage) to a point further forward on the fuselage. Blended into the fuselage and along the wing root, the strake generates a high-speed vortex that remains attached to the top of the wing as the angle of attack increases, generating additional lift and allowing greater angles of attack without stalling. Strakes allow a smaller, lower-aspect-ratio
wing, which increases roll rates and directional stability
while decreasing weight. Deeper wing roots also increase structural strength and internal fuel volume.
Negative stability and fly-by-wire
F-16C of the South Carolina Air National Guard
in-flight over North Carolina equipped with air-to-air missiles, bomb rack, targeting pods and electronic countermeasures pods
The F-16 is the first production fighter aircraft intentionally designed to be slightly aerodynamically unstable, also known as relaxed static stability
(RSS), to improve maneuverability.
Most aircraft are designed with positive static stability, which induces aircraft to return to straight and level flight attitude
if the pilot releases the controls; this reduces maneuverability as the inherent stability has to be overcome. Aircraft with negative
stability are designed to deviate from controlled flight and are thus more maneuverable. At supersonic speeds the F-16 gains stability (eventually positive) due to aerodynamic changes.
To counter the tendency to depart from controlled flight and avoid the need for constant trim inputs by the pilot, the F-16 has a quadruplex (four-channel) fly-by-wire
(FBW) flight control system
(FLCS). The flight control computer (FLCC) accepts pilot input from the stick and rudder controls and manipulates the control surfaces in such a way as to produce the desired result without inducing control loss. The FLCC conducts thousands of measurements per second on the aircraft's flight attitude to automatically counter deviations from the pilot-set flight path; leading to a common aphorism among pilots: "You don't fly an F-16; it flies you."
The FLCC further incorporates limiters governing movement in the three main axes
based on attitude, airspeed and angle of attack (AOA); these prevent control surfaces from inducing instability such as slips
, or a high AOA inducing a stall. The limiters also prevent maneuvers that would exert more than a 9 g
Flight testing has revealed that "assaulting" multiple limiters at high AOA and low speed can result in an AOA far exceeding the 25° limit, colloquially referred to as "departing"; this causes a deep stall; a near-freefall at 50° to 60° AOA, either upright or inverted. While at a very high AOA, the aircraft's attitude is stable but control surfaces are ineffective. The pitch limiter locks the stabilators at an extreme pitch-up or pitch-down attempting to recover. This can be overridden so the pilot can "rock" the nose via pitch control to recover.
Unlike the YF-17, which had hydromechanical
controls serving as a backup to the FBW, General Dynamics took the innovative step of eliminating mechanical linkages from the control stick and rudder pedals to the flight control surfaces
. The F-16 is entirely reliant on its electrical systems to relay flight commands, instead of traditional mechanically linked controls, leading to the early moniker of "the electric jet". The quadruplex design permits "graceful degradation
" in flight control response in that the loss of one channel renders the FLCS a "triplex" system.
The FLCC began as an analog system on the A/B variants but has been supplanted by a digital computer system beginning with the F-16C/D Block 40.
The F-16's controls suffered from a sensitivity to static electricity or electrostatic discharge
(ESD). Up to 70–80% of the C/D models' electronics were vulnerable to ESD.
Cockpit and ergonomics
Bubble canopy, allowing all-round visibility
A key feature of the F-16's cockpit is the exceptional field of view. The single-piece, bird-proof polycarbonate
bubble canopy provides 360° all-round visibility, with a 40° look-down angle over the side of the aircraft, and 15° down over the nose (compared to the common 12–13° of preceding aircraft); the pilot's seat is elevated for this purpose. Furthermore, the F-16's canopy lacks the forward bow frame found on many fighters, which is an obstruction to a pilot's forward vision.
The F-16's ACES IIzero/zero ejection seat
is reclined at an unusual tilt-back angle of 30°; most fighters have a tilted seat at 13–15°. The tilted seat can accommodate taller pilots and increases g
-force tolerance; however, it has been associated with reports of neck ache, possibly caused by incorrect head-rest usage.
Subsequent U.S. fighters have adopted more modest tilt-back angles of 20°.
Due to the seat angle and the canopy's thickness, the ejection seat lacks canopy-breakers for emergency egress; instead the entire canopy is jettisoned prior to the seat's rocket firing.
F-16 ground trainer cockpit (F-16 MLU)
The pilot flies primarily by means of an armrest-mounted side-stick controller (instead of a traditional center-mounted stick
) and an engine throttle; conventional rudder pedals are also employed. To enhance the pilot's degree of control of the aircraft during high-g
combat maneuvers, various switches and function controls were moved to centralized hands on throttle-and-stick
(HOTAS) controls upon both the controllers and the throttle. Hand pressure on the side-stick controller is transmitted by electrical signals via the FBW system to adjust various flight control surfaces to maneuver the F-16. Originally, the side-stick controller was non-moving, but this proved uncomfortable and difficult for pilots to adjust to, sometimes resulting in a tendency to "over-rotate" during takeoffs, so the control stick was given a small amount of "play". Since the introduction of the F-16, HOTAS controls have become a standard feature on modern fighters.
The F-16 has a head-up display
(HUD), which projects visual flight and combat information in front of the pilot without obstructing the view; being able to keep their head "out of the cockpit" improves the pilot's situation awareness
Further flight and systems information are displayed on multi-function displays
(MFD). The left-hand MFD is the primary flight display
(PFD), typically showing radar and moving-maps; the right-hand MFD is the system display (SD), presenting information about the engine, landing gear, slat and flap settings, and fuel and weapons status. Initially, the F-16A/B had monochrome cathode ray tube
(CRT) displays; replaced by color liquid-crystal displays
on the Block 50/52.
The MLU introduced compatibility with night-vision goggles
(NVG). The BoeingJoint Helmet Mounted Cueing System
(JHMCS) is available from Block 40 onwards, for targeting based on where the pilot's head faces, unrestricted by the HUD, using high-off-boresight
missiles like the AIM-9X
The F-16A/B was originally equipped with the Westinghouse AN/APG-66 fire-control radar
. Its slotted planar array
antenna was designed to be compact to fit into the F-16's relatively small nose. In uplook mode, the APG-66 uses a low pulse-repetition frequency
(PRF) for medium- and high-altitude target detection in a low-clutter
environment, and in look-down/shoot-down
employs a medium PRF for heavy clutter environments. It has four operating frequencies within the X band, and provides four air-to-air and seven air-to-ground operating modes for combat, even at night or in bad weather. The Block 15's APG-66(V)2 model added a more powerful signal processing
, higher output power, improved reliability and increased range in cluttered or jamming
environments. The Mid-Life Update (MLU) program introduced a new model, APG-66(V)2A, which features higher speed and more memory.
AN-APG-68, as fitted to the nose
, an evolution of the APG-66, was introduced with the F-16C/D Block 25. The APG-68 has greater range and resolution, as well as 25 operating modes, including ground-mapping, Doppler beam-sharpening, ground moving target indication
, sea target, and track while scan
(TWS) for up to 10 targets. The Block 40/42's APG-68(V)1 model added full compatibility with Lockheed Martin Low-Altitude Navigation and Targeting Infra-Red for Night
(LANTIRN) pods, and a high-PRF pulse-Doppler track mode to provide Interrupted Continuous Wave guidance for semi-active radar-homing
(SARH) missiles like the AIM-7 Sparrow
. Block 50/52 F-16s initially used the more reliable APG-68(V)5 which has a programmable signal processor employing Very-High-Speed Integrated Circuit
(VHSIC) technology. The Advanced Block 50/52 (or 50+/52+) are equipped with the APG-68(V)9 radar, with a 30% greater air-to-air detection range and a synthetic aperture radar
(SAR) mode for high-resolution mapping and target detection-recognition. In August 2004, Northrop Grumman was contracted to upgrade the APG-68 radars of Block 40/42/50/52 aircraft to the (V)10 standard, providing all-weather autonomous detection and targeting for Global Positioning System
(GPS)-aided precision weapons, SAR mapping and terrain-following radar
(TF) modes, as well as interleaving of all modes.
The F-16E/F is outfitted with Northrop Grumman's AN/APG-80 active electronically scanned array
Northrop Grumman developed the latest AESA radar upgrade for the F-16 (selected for USAF and Republic of China Air Force
F-16 upgrades), named the Scalable Agile Beam Radar
In July 2007, Raytheon announced that it was developing a Next Generation Radar (RANGR) based on its earlier AN/APG-79
AESA radar as a competitor to Northrop Grumman's AN/APG-68 and AN/APG-80 for the F-16.
On February 28, 2020, Northrop Grumman received an order from USAF to extend the service lives of their F-16s to at least 2048 with APG-83 Scalable Agile Beam Radar (SABR) as part of the service-life extension program (SLEP).
Afterburner - concentric ring structure inside the exhaust
The initial powerplant selected for the single-engined F-16 was the Pratt & Whitney F100-PW-200 afterburning turbofan
, a modified version of the F-15's F100-PW-100, rated at 23,830 lbf
(106.0 kN) thrust. During testing, the engine was found to be prone to compressor stalls and "rollbacks", wherein the engine's thrust would spontaneously reduce to idle. Until resolved, the Air Force ordered F-16s to be operated within "dead-stick landing
" distance of its bases.
It was the standard F-16 engine through the Block 25, except for the newly built Block 15s with the Operational Capability Upgrade (OCU). The OCU introduced the 23,770 lbf
(105.7 kN) F100-PW-220, later installed on Block 32 and 42 aircraft: the main advance being a Digital Electronic Engine Control (DEEC) unit, which improved reliability and reduced stall
occurrence. Beginning production in 1988, the "-220" also supplanted the F-15's "-100", for commonality. Many of the "-220" engines on Block 25 and later aircraft were upgraded from 1997 onwards to the "-220E" standard, which enhanced reliability and maintainability; unscheduled engine removals were reduced by 35%.
Adjustable exhaust nozzle in contracted position
The F100-PW-220/220E was the result of the USAF's Alternate Fighter Engine (AFE) program (colloquially known as "the Great Engine War"), which also saw the entry of General Electric as an F-16 engine provider. Its F110-GE-100
turbofan was limited by the original inlet to thrust of 25,735 lbf
(114.5 kN), the Modular Common Inlet Duct allowed the F110 to achieve its maximum thrust of 28,984 lbf
(128.9 kN). (To distinguish between aircraft equipped with these two engines and inlets, from the Block 30 series on, blocks ending in "0" (e.g., Block 30) are powered by GE, and blocks ending in "2" (e.g., Block 32) are fitted with Pratt & Whitney engines.)
The Increased Performance Engine (IPE) program led to the 29,588 lbf
(131.6 kN) F110-GE-129 on the Block 50 and 29,160 lbf
(129.4 kN) F100-PW-229 on the Block 52. F-16s began flying with these IPE engines in the early 1990s. Altogether, of the 1,446 F-16C/Ds ordered by the USAF, 556 were fitted with F100-series engines and 890 with F110s.
The United Arab Emirates’ Block 60 is powered by the General Electric F110-GE-132 turbofan with a maximum thrust of 32,500 lbf
(144.6 kN), the highest thrust engine developed for the F-16.
F-16s have participated in numerous conflicts, most of them in the Middle East.
F-16s over Madison
, Wisconsin. The tail of the formation's lead ship features a special 60th Anniversary scheme for the 115th Fighter Wing.
The F-16 had been scheduled to remain in service with the U.S. Air Force until 2025.
Its replacement was planned to be the F-35A variant of the Lockheed Martin F-35 Lightning II
, which is expected to gradually begin replacing several multi-role aircraft among the program's member nations. However, due to delays in the F-35 program, all USAF F-16s will receive service life extension upgrades.
The following year, during the 1982 Lebanon War
Israeli F-16s engaged Syrian aircraft in one of the largest air battles involving jet aircraft, which began on 9 June and continued for two more days. Israeli Air Force F-16s were credited with 44 air-to-air kills during the conflict.
Israeli Air Force F-16I Sufa
On 10 February 2018, an Israeli Air Force F-16I was shot down
in northern Israel when it was hit by a relatively old model S-200
(NATO name SA-5 Gammon) surface-to-air missile of the Syrian Air Defense Force.
The pilot and navigator ejected safely in Israeli territory. The F-16I was part of a bombing mission against Syrian and Iranian targets around Damascus after an Iranian drone entered Israeli air space and was shot down.
An Israel Air Force investigation determined on 27 February 2018 that the loss was due to pilot error since the IAF determined the air crew did not adequately defend themselves.
During the Soviet–Afghan War
, between May 1986 and January 1989, Pakistan Air Force
F-16s shot down at least eight intruders from Afghanistan
. The first three of these (two AfghanSu-22s
and one An-26
) were shot down by two pilots. Pakistani pilots also downed five other intruders (two Su-22s, two MiG-23s
, and one Su-25
Most of these kills were by AIM-9 Sidewinder missiles, but at least one, a Su-22, was destroyed by cannon fire. Flight Lieutenant Khalid Mahmoud is credited with three of these kills. One F-16 was lost in these battles during an encounter between two F-16s and six Afghan aircraft on 29 April 1987; the pilot ejected safely. The downed F-16 was likely hit accidentally
by a Sidewinder fired by the other F-16.
On 7 June 2002, a Pakistan Air Force F-16B Block 15 (S. No. 82-605), flown by Sqn. Leader Zulfiqar, shot down an Indian Air Force unmanned aerial vehicle
, an Israeli-made Searcher II
, using an AIM-9L Sidewinder missile, during a night interception near Lahore
, thus achieving a rare air-to-air kill of a drone at night.
Pakistan Air Force F-16s
The Pakistan Air Force has used its F-16s in various foreign and internal military exercises, such as the "Indus Vipers" exercise in 2008 conducted jointly with Turkey.
On 27 February 2019, two Pakistan Air Force F-16s, one F-16AM Block 15 MLU (S. No. 92731)
, flown by Wg. Cdr. Nauman Ali Khan, Officer Commanding (OC) No. 29 'Aggressor' Squadron, and one F-16BM Block 15 MLU (S. No. 92606)
, flown by Sqn. Ldr. Hassan Mehmood Siddiqui, both aircraft from No. 11 'Arrows' Squadron, reportedly shot down one Indian Air Force
Bison (from No. 51 Squadron, flown by Wg. Cdr. Abhinandan Varthaman
, the Squadron's OC) over Kashmir
India claimed that a Pakistani F-16 was also shot down by the Indian MiG-21 that was shot down after a few minutes,
but the plane crashed in Pakistan administered Kashmir. India also denied loss of any of its Su-30MKI.
Pakistan denied the use or loss of any F-16 during the engagement.
On 28 February 2019, India displayed debris of an AMRAAM missile to show use of F-16s in the mission. Foreign Policy
magazine reported that the US had completed a physical count of Pakistan's F-16s and found none missing.
On 6 April 2019, it was reported that the Pentagon declined to make official statement over any such count.Washington Post
reported that the Pentagon
and the State Department
have yet to issue a public statement on the F-16 count. However, there have been no counter-leaks contradicting the report published by the Foreign Policy.
On 8 April 2019, the IAF released two radar images of aerial engagement to reassert its claims of downing an F-16.
However, Pakistani officials rejected the radar images released by India.
The only confirmed loss from the engagement was the MiG-21.
On 5 April 2019, PAF officials released images of all four missile recovered from the downed MiG-21 to disprove that the aircraft downed the F-16 with a missile.
F-16 SoloTürk aerial aerobatic aircraft
The Turkish Air Force
acquired its first F-16s in 1987. F-16s were later produced in Turkey under four phases of Peace Onyx
programs. In 2015, they were upgraded to Block 50/52+ with CCIP by Turkish Aerospace Industries
Turkish F-16s are being fitted with indigenous AESA radars and EW suite called SPEWS-II.
On 18 June 1992, a Greek Mirage F-1 crashed during a dogfight
with a Turkish F-16.
On 8 February 1995, a Turkish F-16 crashed into the Aegean sea after being intercepted by Greek Mirage F1
On 8 October 1996, seven months after the escalation a Greek Mirage 2000
reportedly fired an R.550 Magic II
missile and shot down a Turkish F-16D over the Aegean Sea
The Turkish pilot died, while the co-pilot ejected and was rescued by Greek forces.
In August 2012, after the downing of a RF-4E
on the Syrian Coast, Turkish Defence Minister İsmet Yılmaz confirmed that the Turkish F-16D was shot down by a Greek Mirage 2000 with an R.550 Magic II in 1996 after violating Greek airspace near Chios
Greece denies that the F-16 was shot down.
Both Mirage 2000 pilots reported that the F-16 caught fire and they saw one parachute
On 23 May 2006, two Greek F-16s intercepted a Turkish RF-4 reconnaissance aircraft and two F-16 escorts off the coast of the Greek island of Karpathos
, within the Athens FIR. A mock dogfight ensued between the two sides, resulting in a midair collision
between a Turkish F-16 and a Greek F-16. The Turkish pilot ejected safely, but the Greek pilot died due to damage caused by the collision.
Five days before the incident, a Turkish F-16 pilot was doing dangerous maneuvers, while being intercepted by Greek F-16 fighters, attempting to hit a Greek fighter.
On 1 March 2020, two Syrian Sukhoi Su-24s
were shot down by Turkish Air Force F-16s using air-to-air missiles
over Syria's Idlib province.
All four pilots safely ejected.
On 3 March 2020, a Syrian Arab Army Air Force L-39
combat trainer was shot down by a Turkish F-16 over Syria's Idlib province.
The pilot died.
As a part of Turkish F-16 modernization program new air to air missiles are being developed and tested for the aircraft. GÖKTUĞ
program led by TUBITAK SAGE
has presented two types of air to air missiles named as Bozdogan (Merlin
) and Gokdogan (Peregrine
). While Bozdogan has been categorized as a Within Visual Range Air-to-Air Missile (WVRAAM), Gokdogan is a Beyond Visual Range Air-to-Air-Missile (BVRAAM
). On April 14, 2021, first live test exercise of Bozdogan have successfully completed and the first batch of missiles are expected to delivered throughout the same year to the Turkish Air Force.
On 16 February 2015, Egyptian F-16s struck jihadi weapons caches and training camps in Libya
in retaliation for the murder of 21 Egyptian Coptic Christian construction workers by masked militants affiliated with the Islamic State (ISIS). The air strikes killed 64 ISIS fighters, including three leaders in Derna and Sirte on the coast.
A Yugoslavian MiG-29
was shot down by a Dutch F-16AM during the Kosovo War
Belgian and Danish F-16s also participated in joint operations over Kosovo during the war.
Dutch, Belgian, Danish, and Norwegian F-16s were deployed during the 2011 intervention in Libya
and in Afghanistan.
In Libya, Norwegian F-16s dropped almost 550 bombs and flew 596 missions,
some 17% of the total strike missions
including the bombing of Muammar Gaddafi's headquarters.
In late March 2018, Croatia announced its intention to purchase 12 used Israeli F-16C/D "Barak"/"Brakeet" jets, pending U.S. approval.
Acquiring these F-16s would allow Croatia to retire its aging MiG-21s
On 11 July 2018, Slovakia's government approved the purchase of 14 F-16s Block 70/72 to replace its aging fleet of Soviet-made MiG-29s
A contract was signed on 12 December 2018 in Bratislava.
A Portuguese Air Force
F-16A outfitted with AIM-9 Sidewinder missiles, AN/ALQ-131 ECM pod, and external fuel tanks.
F-16 models are denoted by increasing block numbers
to denote upgrades. The blocks cover both single- and two-seat versions. A variety of software, hardware, systems, weapons compatibility, and structural enhancements have been instituted over the years to gradually upgrade production models and retrofit
The F-16A (single seat) and F-16B (two seat) were initial production variants. These variants include the Block 1, 5, 10 and 20 versions. Block 15 was the first major change to the F-16 with larger horizontal stabilizers. It is the most numerous of all F-16 variants with 475 produced.
Many F-16A and B aircraft have been upgraded to the Mid-Life Upgrade (MLU) Block 20 standard, becoming functionally equivalent to mid-production C/D models.
The F-16C (single seat) and F-16D (two seat) variants entered production in 1984. The first C/D version was the Block 25 with improved cockpit avionics and radar which added all-weather capability with beyond-visual-range
(BVR) AIM-7 and AIM-120 air-air missiles. Block 30/32, 40/42, and 50/52 were later C/D versions.
The F-16C/D had a unit cost of US$18.8 million (1998). Operational cost
per flight hour has been estimated at $7,000
or $24,000, depending on calculation method.
For the Indian MRCA competition
for the Indian Air Force
, Lockheed Martin offered the F-16IN Super Viper
The F-16IN is based on the F-16E/F Block 60 and features conformal fuel tanks; AN/APG-80 AESA radar, GE F110-GE-132A engine with FADEC
controls; electronic warfare suite and Infra-red search and track (IRST)
unit; updated glass cockpit; and a helmet-mounted cueing system.
As of 2011, the F-16IN is no longer in the competition.
In 2016, Lockheed Martin offered the new F-16 Block 70/72 version to India under the Make in India
In 2016, Indian government offered to purchase 200 (potentially up to 300) fighters in a deal worth $13–15bn.
As of 2017, Lockheed Martin has agreed to manufacture F-16 Block 70 fighters in India with the Indian defense firm Tata Advanced Systems Limited. The new production line could be used to build F-16s for India and for exports.
The F-16N was an adversary aircraft operated by the U.S. Navy
. It is based on the standard F-16C/D Block 30 and is powered by the General Electric F110-GE-100 engine, and is capable of supercruise
The F-16N has a strengthened wing and is capable of carrying an Air Combat Maneuvering Instrumentation (ACMI) pod on the starboard wingtip. Although the single-seat F-16Ns and twin-seat (T)F-16Ns are based on the early-production small-inlet Block 30 F-16C/D airframe, they retain the APG-66 radar of the F-16A/B. In addition, the aircraft's 20 mm cannon has been removed, as has the ASPJ, and they carry no missiles. Their EW fit consists of an ALR-69 radar warning receiver (RWR) and an ALE-40 chaff/flare dispenser. The F-16Ns and (T)F-16Ns have the standard Air Force tailhook and undercarriage and are not aircraft carrier capable. Production totaled 26 airframes, of which 22 are single-seat F-16Ns and four are twin-seat TF-16Ns. The initial batch of aircraft were in service between 1988 and 1998. At that time, hairline cracks were discovered in several bulkheads and the Navy did not have the resources to replace them, so the aircraft were eventually retired, with one aircraft sent to the collection of the National Naval Aviation Museum
at NAS Pensacola
, Florida, and the remainder placed in storage at Davis-Monthan AFB
. These aircraft were later replaced by embargoed ex-Pakistani F-16s in 2003. The original inventory of F-16Ns were previously operated by adversary squadrons at NAS Oceana
, Virginia; NAS Key West
, Florida and the former NAS Miramar
, California. The current F-16A/B aircraft are operated by the Naval Strike and Air Warfare Center
at NAS Fallon
At the 2012 Singapore Air Show Lockheed Martin unveiled plans for the new F-16V variant with the V suffix for its Viper nickname. It features an AN/APG-83 active electronically scanned array
(AESA) radar, a new mission computer and electronic warfare suite, automated ground collision avoidance system, and various cockpit improvements; this package is an option on current production F-16s and can be retrofitted to most in service F-16s.
First flight took place 21 October 2015.
Lockheed and AIDC
both invested in the development of the aircraft and will share revenue from all sales and upgrades.
Upgrades to Taiwan's F-16 fleet began in January 2017.
The first country to confirm the purchase of 16 new F-16V Block 70/72 was Bahrain.
Slovakia announced on 11 July 2018 that it intends to purchase 14 F-16V Block 70/72 aircraft.
Lockheed Martin has redesignated the F-16V Block 70 as the "F-21" in its offering for India's fighter requirement.
The Republic of China Air Force
announced on 19 March 2019 that it formally requested the purchase of an additional 66 F-16V jets.
administration approved the sale on 20 August 2019.
On 14 August 2020, Lockheed Martin was awarded a US$
62 billion contract by the US DoD
that includes 66 new F-16s at US$8 billion for Taiwan.
USAF QF-16A, on its first unmanned test flight, over the Gulf of Mexico
Map with F-16 operators in blue with former operator in red
By July 2010, there had been 4,500 F-16s delivered.
Notable accidents and incidents
The F-16 has been involved in over 670 hull-loss accidents as of January 2020.
- On 8 May 1975, while practicing a 9-g aerial display maneuver with the second YF-16 (tail number 72-1568) at Fort Worth, Texas, prior to being sent to the Paris Air Show, one of the main landing gears jammed. The test pilot, Neil Anderson, had to perform an emergency gear-up landing and chose to do so in the grass, hoping to minimize damage and to avoid injuring any observers. The aircraft was only slightly damaged, but due to the mishap the first prototype was sent to the Paris Air Show in its place.
- On 15 November 1982, while on a training flight outside Kunsan Air Base in South Korea, USAF Captain Ted Harduvel died when he crashed inverted into a mountain ridge. In 1985, Harduvel's widow filed a lawsuit against General Dynamics claiming an electrical malfunction, not pilot error, as the cause; a jury awarded the plaintiff $3.4 million in damages. However, in 1989, the U.S. Court of Appeals ruled the contractor had immunity to lawsuits, overturning the previous judgment. The court remanded the case to the trial court "for entry of judgment in favor of General Dynamics". The accident and subsequent trial was the subject of the 1992 film Afterburn.
- On 23 March 1994, during a joint Army-Air Force exercise at Pope AFB, North Carolina, F-16D (AF Serial No. 88-0171) of the 23d Fighter Wing / 74th Fighter Squadron was simulating an engine-out approach when it collided with a USAF C-130E. Both F-16 crew members ejected, but their aircraft, on full afterburner, continued on an arc towards Green Ramp and struck a USAF C-141 that was being boarded by US Army paratroopers. This accident resulted in 24 fatalities and at least 100 others injured. It has since been known as the "Green Ramp disaster".
- On 10 March 1997 at 1330 hrs, an Indonesian Air Force F-16A Block 15 #TS-1607 from the 3rd Squadron crashed at the Halim AB in Jakarta while attempting to land during bad weather and crashed into the landing lights for the runway, killing the pilot, Captain Dwi Sasongko of the local demonstration team 'Blue Eagle.
- On 15 September 2003, a USAF Thunderbird F-16C crashed during an air show at Mountain Home AFB, Idaho. Captain Christopher Stricklin attempted a "Split S" maneuver based on an incorrect mean-sea-level altitude of the airfield. Climbing to only 1,670 ft (510 m) above ground level instead of 2,500 ft (760 m), Stricklin had insufficient altitude to complete the maneuver, but was able to guide the aircraft away from spectators and ejected less than one second before impact. Stricklin survived with only minor injuries; the aircraft was destroyed. USAF procedure for demonstration "Split-S" maneuvers was changed, requiring both pilots and controllers to use above-ground-level (AGL) altitudes.
- On 26 January 2015, a Greek F-16D crashed while performing a NATO training exercise in Albacete, Spain. Both crew members and nine French soldiers on the ground died when it crashed in the flight-line, destroying or damaging two Italian AMXs, two French Alpha jets, and one French Mirage 2000.
- On 16 April 2015, an Indonesian Air Force F-16 Block 25 #TS-1643 from the 3rd Squadron caught fire and burnt prior to taking off at Halim Perdanakusuma AFB, Jakarta. The pilot escaped.
- On 24 June 2015, an Indonesian Air Force F-16A Block 15 # TS-1609 from the 3rd Squadron crashed into the runway at Iswahyudi AFB in East Java, Indonesia. The pilot recovered and the aircraft was repaired.
- On 7 July 2015, an F-16CJ collided with a Cessna 150M over Moncks Corner, South Carolina, U.S. The pilot of the F-16 ejected safely, but both people in the Cessna were killed.
- On 14 March 2017 , an Indonesian Air Force F-16B Block 15 #TS-1603 from the 3rd Squadron skidded off the runway after a brake failure at the Roesmin Nurjadin AFB. Both pilots recovered.
- On 20 February 2018, an F-16CM experienced an engine fire on takeoff, necessitating an immediate landing back at Misawa AB, Japan. Assigned to the 13th Fighter Squadron, of the 35th Fighter Wing, the aircraft sustained engine damage and loss of external fuel tanks with an estimated governmental loss of $987,545.57 (equivalent to $1,005,475 in 2019). The primary cause was an obsolete part installed on an incompatible bracket during an overhaul in 2012.[importance?]
- On 11 October 2018, an F-16 MLU from the 2nd Tactical Wing of the Belgian Air Component, on the apron at Florennes Air Station, was hit by a gun burst from a nearby F-16, whose canon was fired inadvertently during maintenance. The aircraft caught fire and was burned to the ground, while two other F-16s were damaged and two maintenance personnel were treated for aural trauma.
Aircraft on display
- J-215 of the RNLAF on display at the National Military museum at former airbase Soesterberg.
- J-228 of the RNLAF on pylon display at the Leeuwarden Airbase Main Gate entry road.
- J-240 of the RNLAF on pylon display past the Volkel Airbase Main Gate on the entry road.
- J-246 of the RNLAF on pylon display on the N264 / Zeelandsedijk roundabout near the Volkel Airbase Main Gate entry.
YF-16A (Full-Scale Development)
- 75-0745 – Used as a traveling exhibit, on loan from the National Museum of the United States Air Force, Wright-Patterson AFB, Ohio
- 75-0746 – Pylon-mounted gate guard, McEntire Air National Guard Base, South Carolina
- 75-0748 – Cadet Area Terrazzo, U.S. Air Force Academy, Colorado
- 75-0750 – Experimental Aircraft Display Hangar, National Museum of the United States Air Force, Wright-Patterson AFB, Ohio
- 78-0001 – Langley AFB Memorial Park, Langley AFB, Virginia. First production model F-16A delivered to USAF.
- 78-0005 – 162d Fighter Wing Park, Tucson Air National Guard Base, Arizona
- 78-0025 – Valiant Air Command Warbird Museum, Titusville, FL. Formerly a gate guard, Burlington Air National Guard Base, Vermont
- 78-0042 – Gate guard, Montgomery Air National Guard Base/Dannelly Field, Alabama
- 78-0052 – Eielson AFB Heritage Park, Eielson AFB, Alaska
- 78-0059 – Selfridge Military Air Museum and Air Park, Selfridge ANGB, Michigan
- 78-0061 - Highland Home "Flying Squadron" High School Football Field, Highland Home, Alabama
- 78-0065 – 388th Fighter Wing and 419th Fighter Wing combined Headquarters, Hill AFB, Utah
- 78-0066 – On display in Kansas Air National Guard Memorial Park area, McConnell AFB, Kansas
- 79-0290 – On display at Great Falls Air National Guard Base, Montana.
- 79-0296 – Gate guard, Jacksonville Air National Guard Base, Florida
- 79-0307 – On display at Cannon AFB Air Park, Cannon AFB, New Mexico
- 79-0309 – Base park area adjacent to USAFCENT Headquarters, Shaw AFB, South Carolina. Painted as 20th Fighter Wing F-16C 93–0534. Memorial to Maj Brinson Phillips, 20 FW, killed 19 March 2000 while flying F-16C 93-0534
- 79-0312 – On pylon display, 8th Street Park, Douglas, Arizona
- 79-0326 – Gate guard, Homestead Air Reserve Base, Florida
- 79-0327 – Pedestal mounted memorial, Luke AFB, Arizona. Painted in 302d Fighter Squadron markings, to include World War IITuskegee Airmen "Red Tails" empennage
- 79-0334 – USS Alabama Battleship Memorial Park, Mobile, Alabama
- 79-0337 – Ground-mobile static display aircraft, normally located at Hancock Field Air National Guard Base, New York. Used by New York Air National Guard's 174th Attack Wing (former 174th Fighter Wing) at fairs and expositions for Air National Guard recruiting.
- 79-0352 – On static display with 23d Wing at Moody AFB, Georgia
- 79-0366 – Memorial park static display, Mountain Home AFB, Idaho
- 79-0373 – On display at Buckley AFB, Colorado. Aircraft painted in markings of Colorado Air National Guard's 140th Fighter Wing based at Buckley AFB.
- 79-0388 – Hill Aerospace Museum, Hill AFB, Utah
- 79-0402 – Hill Aerospace Museum, Hill AFB, Utah
- 79-0403 – Intrepid Sea, Air & Space Museum, New York City, New York
- 80-0481 – Display on Parade Ground, Sheppard AFB, Texas.
- 80-0527 – Former Arizona Air National Guard162d Fighter Wing aircraft destined for transfer to/display at the Pima Air and Space Museum, Tucson, Arizona.
- 80-0528 – City park in Pinellas Park, Florida. Painted in markings of 56th Tactical Training Wing-cum-56th Fighter Wing, previously assigned to nearby MacDill AFB in the 1980s and early 1990s.
- 80-0573 – Air Force Armament Museum, Eglin AFB, Florida.
- 80-0612 – Memorial park static display at Puerto Rico National Guard's Camp Santiago, Salinas, Puerto Rico. Former Puerto Rico Air National Guard F-16ADF, painted in markings of PRANG's former 198th Fighter Squadron, but marked as 81612.
- 81-0663 – On display in United States Air Force Thunderbirds markings at the National Museum of the United States Air Force, Wright-Patterson AFB, Dayton, Ohio.
- 81-0676 – Museum of Aviation, Robins AFB, Warner Robins, Georgia
- 81-0721 – MacDill AFB Memorial Park, MacDill AFB, Florida. Former Florida Air National Guard 125th Fighter Wing F-16ADF repainted in markings of a 56th Fighter Wing F-16A previously assigned to MacDill in the 1980s.
- 81-0807 – On display at Minnesota Air National Guard Museum, Saint Paul, Minnesota.
- 82-0926 – On display at Fargo Air National Guard Base, Fargo, North Dakota.
- 82-0930 – On display at Ellington Field Joint Reserve Base, Houston, Texas
- 78-0088 – On display at the Naval Air Station Wildwood Aviation Museum, Cape May County Airport, New Jersey
- 78-0101 – On display at United States Space Camp / Aviation Challenge, Huntsville, Alabama
- 78-0107 – On display adjacent to Parade Ground, Lackland AFB, Texas
- 79-0430 – Stafford Air & Space Museum, Weatherford, Oklahoma
- 80-0633 – Yanks Air Museum, Chino, California.
- 81-0816 – Pylon display gate guard, Atlantic City Air National Guard Base, New Jersey
- 81-0817 – Russell Military Museum, Russell, Illinois.
- 83-1126 – Pylon display at Hill Memorial Park, Hill AFB, Utah
- 84-1264 – Air park display, Fort Wayne Air National Guard Station, Indiana. Aircraft retains Air Force Heritage paint scheme honoring 358th Fighter Group during World War II.
- 84-1393 – Pylon display at Texas National Guard's Camp Mabry, Austin, Texas. Former Texas Air National Guard 147th Fighter Wing/111th Fighter Squadron aircraft.
- 85-1469 – Static display at Joe Foss Field Air National Guard Station, South Dakota
- 87-0255 – On display adjacent to 149th Fighter Wing, Lackland AFB, Texas
- 87-0323 – Preserved as Thunderbird 1 in front of the USAF Air Demonstration Squadron/United States Air Force Thunderbirds hangar, Nellis AFB, Nevada. Assigned to Thunderbirds in the 1992–2008 timeframe. Had number 1 attached on 11 June 1999; number 2 in the 2004 season; number 3 on 3 March 2003 and number 4 on 1 April 2005.
- 163269 – San Diego Aerospace Museum, San Diego, California
- 163271 – Pacific Coast Air Museum, Santa Rosa, California
- 163277 – Palm Springs Air Museum, Palm Springs, California
- 163569 – NAS Fort Worth JRB, Fort Worth, Texas. It is painted in USAFR colors of the 457th FS, 301st FW.
- 163572 – National Naval Aviation Museum, Naval Air Station Pensacola, Pensacola, Florida
- 163576 – Air Power Park, Naval Air Station Fallon, Nevada
Specifications (F-16C Block 50 and 52)
3-view drawing of F-16
View of underside of F-16 during a vertical climb
- Crew: 1
- Length: 49 ft 5 in (15.06 m)
- Wingspan: 32 ft 8 in (9.96 m)
- Height: 16 ft (4.9 m)
- Wing area: 300 sq ft (28 m2)
- Airfoil: NACA 64A204
- Empty weight: 18,900 lb (8,573 kg)
- Gross weight: 26,500 lb (12,020 kg)
- Max takeoff weight: 42,300 lb (19,187 kg)
- Fuel capacity: 7,000 pounds (3,200 kg) internals
- Powerplant: 1 × General Electric F110-GE-129 afterburning turbofan (for Block 50 version), 17,155 lbf (76.31 kN) thrust dry, 29,500 lbf (131 kN) with afterburner
- Powerplant: 1 × Pratt & Whitney F100-PW-229 afterburning turbofan (for Block 52 version), 17,800 lbf (79 kN) thrust dry, 29,560 lbf (131.5 kN) with afterburner
- Maximum speed: Mach 2.05 1,145 kn (1,318 mph; 2,121 km/h) at 40,000 feet, clean
Mach 1.2, 800 kn (921 mph; 1,482 km/h) at sea level
- Combat range: 295 nmi (339 mi, 546 km) on a hi-lo-hi mission with 4 × 1,000 lb (454 kg) bombs
- Ferry range: 2,277 nmi (2,620 mi, 4,217 km) with drop tanks
- Service ceiling: 60,000 ft (18,000 m) (maintains 500 ft/min climb potential at 60000 feet according to the Supplement of F-16C/D Flight Manual.)
- g limits: +9.0
- Roll rate: 324°/s
- Rate of climb: 72,000 ft/min (370 m/s) (sustains 72,000 ft/min in 4.2g ascending turn)[N 2]
- Wing loading: 88.3 lb/sq ft (431 kg/m2)
- Thrust/weight: 1.095 (1.24 with loaded weight & 50% internal fuel)
- Guns: 1 × 20 mm (0.787 in) M61A1 Vulcan 6-barrel rotary cannon, 511 rounds
- Hardpoints: 2 × wing-tip air-to-air missile launch rails, 6 × under-wing, and 3 × under-fuselage pylon (2 of 3 for sensors) stations with a capacity of up to 17,000 lb (7,700 kg) of stores,
- 4 × LAU-61/LAU-68 rocket pods (each with 19/7 × Hydra 70 mm/APKWS rockets, respectively)
- 4 × LAU-5003 rocket pods (each with 19 × CRV7 70 mm rockets)
- 4 × LAU-10 rocket pods (each with 4 × Zuni 127 mm rockets)
Notable appearances in media
- ^ Note that the F-16XL was originally referred to as "F-16E", with "F-16F" reserved for a variant, however this was dropped after the decision was made to procure the F-15E Strike Eagle instead.
- ^ According to Figure B8-37 of F-16C/D Flight Manual.
- ^ a b Weisgerber, Marcus (22 March 2007). "Lockheed to Move F-16 Production to South Carolina". Defense One. Archived from the original on 23 June 2018. Retrieved 28 June 2018.
- ^ "How the F-16 fighter jet put Fort Worth on the aerospace map". star-telegram.com. Archived from the original on 24 November 2017. Retrieved 24 November 2017.
- ^ a b "Lockheed Martin Awarded Contract to Build F-16 Block 70 Aircraft for Bahrain". Archived from the original on 29 June 2018. Retrieved 28 June 2018.
- ^ "Lockheed Martin to deliver 4,500th F-16 fighter". McClatchy DC. 2 April 2012. Archived from the original on 31 July 2014. Retrieved 13 September 2014.
- ^ "F-16 Fighting Falcon – International Users". Global Security. Archived from the original on 24 August 2011. Retrieved 2 February 2016.
- ^ Rosenwald, Michael S. "Downside of Dominance? Popularity of Lockheed Martin's F-16 Makes Its F-35 Stealth Jet a Tough Sell."Archived 14 October 2017 at the Wayback Machine Washington Post, updated 17 December 2007. Retrieved 11 July 2008.
- ^ "Company Histories – Lockheed Martin Corporation". Funding universe. Archived from the original on 17 April 2012. Retrieved 13 September 2014.
- ^ Aleshire 2005, p. xxii.
- ^ Peacock 1997, p. 100.
- ^ Stout, Joe and Laurie Quincy. "United States Government Awards Lockheed Martin Contract to Begin Production of Advanced F-16 Aircraft for Morocco." Archived 4 January 2009 at the Wayback Machine Lockheed Martin press release, 8 June 2008. Retrieved 11 July 2008.
- ^ "Strength in numbers: The World's Top 10 military aircraft types". Flight global. Reed Business Information. 9 January 2015. Archived from the original on 17 November 2015. Retrieved 30 October 2015.
- ^ Spick 2000, p. 190.
- ^ Hillaker, Harry. "John Boyd, USAF Retired, Father of the F-16". Archived from the original on 1 June 2009. Retrieved 7 June 2008. Code One: An Airpower Projection Magazine, April/July 1997. Retrieved 21 August 2011.
- ^ Code One, April & July 1991. Retrieved 21 August 2011.
- ^ Richardson 1990, pp. 7–8.
- ^ Coram 2002, pp. 245–46.
- ^ Bjorkman, Eileen, Small fast and in your face, Air & Space, Feb/March 2014, pp. 28–35
- ^ Peacock 1997, pp. 9–10.
- ^ Richardson 1990, pp. 7–9.
- ^ Peacock 1997, pp. 10–11.
- ^ Richardson 1990, pp. 8–9.
- ^ Martin, Douglas. "Robert H. Widmer, Designer of Military Aircraft, Dies at 95." Archived 28 December 2016 at the Wayback Machine The New York Times, 2 July 2011.
- ^ Richardson 1990, pp. 12–13.
- ^ Jenkins 2000, p. 14.
- ^ Osborne, Phil, Executive Producer. "F-16 Fighting Falcon" (video #9-315842-037444). Magna Pacific, 2009. Quote: At 17:29, "Another development, which both manufacturers were aware of, was the aging F-104 Starfighters, which equip several European NATO air forces, would soon need to be replaced."
- ^ Jenkins 2000, pp. 14–15, 19–20.
- ^ a b Richardson 1990, p. 14.
- ^ a b Peacock 1997, pp. 12–13.
- ^ "YF-16 The Birth of a Fighter". f-16.net. Archived from the original on 9 July 2017. Retrieved 29 June 2017.
- ^ Dörfer, Ingemar. "The Selling of the F-16."Archived 17 September 2011 at the Wayback Machine Foreignaffairs.com, 1983. Retrieved: 23 April 2011.
- ^ Coram 2002, p. 305.
- ^ Peacock 1997, pp. 13–16.
- ^ Richardson 1990, p. 13.
- ^ Peacock 1997, pp. 14, 17–19, 33–34.
- ^ Donald, David ed. "Boeing F/A-18 Hornet". Warplanes of the Fleet. London: AIRtime, 2004. ISBN 1-880588-81-1.
- ^ Darling 2003, p. 17.
- ^ Peacock 1997, pp. 31–32.
- ^ Spick 2000, p. 196.
- ^ Peacock 1997, pp. 17–19, 33–34.
- ^ Peacock 1997, pp. 14–16, 21.
- ^ Richardson 1990, pp. 13–15.
- ^ a b c d e f g h i j "Lockheed Martin F-16 Fighting Falcon." Jane's All The World's Aircraft, updated 21 January 2008. Retrieved: 30 May 2008.
- ^ Fuquay, Jim. "Iraq to buy 18 more Lockheed F-16 fighters." Archived 13 December 2013 at the Wayback Machine Star-Telegram, 1 May 2013.
- ^ Chambers, Joseph R. "Lockheed Martin F-16 Fighting Falcon: Curing Deep Stall", Partners in Freedom: Contributions of the Langley Research Center to U.S. Military Aircraft of the 1990s."; Monographs in Aerospace History Number 19, The NASA History Series (NASA SP-2000-4519). Archived 20 August 2008 at the Wayback Machine National Aeronautics and Space Administration, Washington, DC, 2000. Retrieved: 22 June 2008.
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