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The Vickers Valiant was a British high-altitude jet bomber designed to carry nuclear weapons, and in the 1950s and 1960s was part of the Royal Air Force's "V bomber" strategic deterrent force. It was developed by Vickers-Armstrongs in response to Specification B.35/46 issued by the Air Ministry for a nuclear weapon jet-powered bomber. The Valiant was the first of the V bombers to become operational, and was followed by the Handley Page Victor and the Avro Vulcan. The Valiant is the only V bomber to have dropped live nuclear weapons (for test purposes).Blackman and Wright 2015, p. 33.
In 1956, Valiants operating from Malta flew conventional bombing missions over Egypt for Operation Musketeer during the Suez Crisis. From 1956 until early 1966 the main Valiant force was used in the nuclear deterrence role in the confrontation between NATO and the Warsaw Pact powers. Other squadrons undertook aerial refuelling, aerial reconnaissance and Electronic Warfare.
In 1962, in response to advances in Soviet Union surface-to-air missile (SAM) technology, the V-force fleet including the Valiant changed from high-level flying to flying at low-level to avoid high altitude SAM attacks. In 1964 it was found that Valiants showed fatigue and crystalline corrosion in wing rear spar attachment forgings. In late 1964 a repair programme was underway, but a change of Government led to the new Minister of Defence Denis Healey deciding that the Valiant should be retired from service, and this happened in early 1965. The Victor and Vulcan V-bombers remained in service until the 1980s.
In January 1947, the British Air Ministry issued Specification B.35/46 for an advanced jet bomber intended to carry nuclear weapons and to fly near the speed of sound at altitudes of . Three firms: Avro, Handley-Page and Vickers-Armstrongs submitted advanced designs intended to meet the stringent requirements.Burnet and Morgan Aeroplane Monthly August 1980, p. 397. While Short Brothers submitted a design, by Geoffrey T. R. Hill, that was judged too ambitious, the Air Staff accepted another submission from the company for a separate requirement, B.14/46, as "insurance" in case the advanced B.35/46 effort ran into trouble. Aviation authors Bill Gunston and Peter Gilchrist described Specification B.14/46 as "calling for little more than a traditional aircraft fitted with jet engines"Gunston and Gilchrist 1993, p. 72. Short submitted a conservative design to meet B.14/46, which became the Short Sperrin. Two prototypes were completed, the first conducting its maiden flight in 1951, but the Sperrin was ultimately relegated to research and development purposes only.
Vickers had emerged from World War II as one of the world's pre-eminent companies in the field of aeronautical manufacturing and development. The company operated its own secretive Skunk Works-like development organisation based at Weybridge, Surrey, which had been involved in several secret wartime development projects. It was this secretive division where the early development of the Valiant took place, including the later assembly of the initial two prototypes.Gunston and Gilchrist 1993, pp. 72–73. Vickers initially produced a six-engine jet bomber design proposal to meet Specification B.35/46. As progress in the development of more powerful jet engines was made, this was re-worked to a four-engine proposal in 1948.Gunston and Gilchrist 1993, p. 73. The proposed design submitted by Vickers was relatively straightforward, being less aerodynamically advanced in comparison to competing bids made by rival firms.Blackman and Wright 2015, p. 17.
Both Handley-Page and Avro had produced advanced designs for the bomber competition. These were produced as the Victor and the Avro Vulcan respectively. The Air Staff decided to award contracts to each company as a form of insurance in case one of the designs failed. The submissions became known as the , or V-class, with the aircraft given names that started with the letter "V".Downey 1985, p. 5. Vickers' submission had initially been rejected as not being as advanced as the Victor and the Vulcan,Rosemeyer 2009, p. 52. but Vickers' chief designer George Edwards lobbied the Air Ministry on the basis that it would be available much sooner than the competition, going so far as to promise that a prototype would be flown by the end of 1951, that subsequent production aircraft would be flown prior to the end of 1953, and that serial deliveries would commence during early 1955. Gaining the bomber contract was considered of crucial importance to the future of aircraft manufacturing at Vickers. "Edwards was supremely confident that Weybridge could deliver the aircraft as specified .. " and "..committed to the brochure performance figures and dates because he thought they knew how to do it". He resisted being pushed to try to more closely match the Victor and Vulcan height and speed requirements or to change equipment from that originally specified as these distractions would jeopardize his promised delivery dates.Gardner 2006, p. 92.
Although developing three different aircraft types in response to a single Operational Requirement (OR) was costly, events such as the Berlin Blockade had led to a sense of urgency in providing a deterrent to the Soviet Union from possible acts of aggression in Western Europe.Rosemeyer 2009, pp. 52–53.
In April 1948, the Air Staff issued a specification with the designation B.9/48 written around the Type 660 Vickers design; and an 'Instruction to Proceed' was received by Vickers on 16 April 1948.
In February 1949, two prototypes of the Vickers 660 series were ordered. The first was to be fitted with four Rolls-Royce Rolls-Royce Avon turbojet engines, while the second was to be fitted with four Armstrong Siddeley Sapphire engines and was designated the Type 667.Andrews and Morgan 1988, p. 438.
On 11 January 1952, the first Valiant prototype was lost while making internal noise measurements for the V.1000 programme. Testing included engine shutdowns and re-lights,Andrews 1965, p. 4. one of which caused a fire in the starboard wing; most of the crew managed to escape the aircraft safely, except for the co-pilot, who struck the tail after ejecting. Flight 4 July 1958, p. 13.Blackman and Wright 2015, pp. 11–16.
On 11 April 1952, the second prototype WB215 made its maiden flight, after modifications to the fuel system.Andrews and Morgan 1988, p. 440. It was fitted with more powerful RA.7 Avon engines with thrust each, rather than the originally planned Sapphires. It also featured more rounded air inlets, replacing the narrow slot-type intakes of the first prototype, to feed sufficient air to the more powerful engines. The short delay until the second prototype became available meant that loss of the prototype did not compromise the development schedule.Turpin 2002, p. 74.Jones 2007, p. 34.
The prototype B.2, serial number WJ954 first flew on 4 September 1953.Andrews and Morgan 1988, p. 445. Finished in a gloss black night operations paint scheme, it became known as the "Black Bomber". Its performance at low level was superior to that of the B.1 (or any other V-bomber), particularly at sea level, with the aircraft being cleared for at low level (with speeds of up to being reached in testing). This was compared to the B.1 sea-level limit of . The Air Ministry ordered 17 production B.2 aircraft, which were to be powered by Rolls-Royce Conway . Although the Valiant B.2 low-level capabilities were significant, the programme was terminated because the World War 2 "Pathfinder concept" was considered obsolete in the nuclear era.Gunston and Gilchrist 1993, p. 78. The B.2 prototype was used for tests for a few years, including the clearance of rocket-assisted take-offs, for the Valiant B.1 at hot or high airfields, using two Super-Sprite rocket motors. It also did extensive taxiing tests to investigate the cause of brake judder which caused a fatigue failure of the landing gear. It was scrapped in 1958.Trubshaw and Edmondson 1998, p. 37.Jones 2007, pp. 36–37.Brookes 2012, pp. 83–84.
On 8 February 1955, this first production Valiant was delivered to the RAF.Brookes 2012, p. 12.Flintham 2008, p. 131. Britain's "V-bomber" force, as it had been nicknamed in October 1952, formally entered operational service on that day. The Victor and Vulcan would soon follow the Valiant into service, for a total of three types of nuclear-armed strategic bombers in RAF service. In September 1957, the final Valiant was delivered. All production aircraft had been delivered on time and below budget.
A total of 108 Valiants were manufactured, including the sole B.2 prototype. In addition to its principal role as part of Britain's nuclear deterrent, the Valiant bomber also dropped high explosive bombs. The bombers were followed into service by a strategic reconnaissance version and a multi-purpose version capable conventional bombing, aerial reconnaissance and aerial refueling. 18 squadron operated 6 Valiants with electronic countermeasures equipment.Blackman and Wright 2015, pp. 19–20. Valiants of 90 and 214 squadrons were used for air refuelling through the addition of a Hose Drum Unit (HDU) in the bomb bay, mounted on the same suspension units that were also used for bombs. This meant that for refuelling, the bomb-bay doors had to be opened so that the refuelling hose could be streamed (unlike later tankers where the HDU was flush with the under fuselage rather than inside a bomb bay). Several Valiants were also used for testing and development purposes, such as its use as a flying testbed during trials of the Blue Steel nuclear-armed standoff missile, which was later added to the arsenal of munitions the other V-bombers were equipped with.Blackman and Wright 2015, pp. 24–26.Flintham 2008, p. 133.
Unlike the Vulcan and Victor, the Valiant did not see the production of a more capable mark 2 model. In 1962 the Valiant bomber squadrons were switched to a low-level flight profile in order to avoid enemy Surface-to-Air (SAM) defence systems. In 1964 fatigue was discovered due to the increased air turbulence in low level flying and led to the type's premature retirement. Vic Flintham observed that: "There is a fine irony to the situation, for Vickers had produced the Type 673 B Mk 2 version designed as a fast, low-level pathfinder... The Air Ministry was not interested..." The Valiant was Vickers' last purpose-built military aircraft. It was followed by the Vickers Vanguard, a passenger turboprop designed in 1959, and the Vickers VC10, a jet passenger aircraft in 1962, also used as a military transport and tanker by the RAF.
The wing of the Valiant used a "compound sweep" configuration, devised by Vickers aerodynamics Elfyn Richards.Barfield Air International September 1992, p. 158. Richards found that it was necessary to increase the sweep on the inboard section of the wing, a discovery which he later as "Improvements in Aeroplane Wing Formation" with an explanation that "the formation of the shockwaves be delayed to the same extent over the whole span of the wing";Patent Specification 631,785, Improvements in Aeroplane Wing Formation", Elfyn John Richards, Application Date Nov. 25,1947 the Valiant wing had 37° sweepback for the inner third of the wing, and 21° for the remainder.Burnet and Morgan Aeroplane Monthly August 1980, p. 398.Gunston and Gilchrist 1993, p. 74. This was because the thickness/chord ratio could be reduced closer to the tips. The choice to have mild sweepback around the aerodynamic control surfaces meant that in-service speeds were limited to Mach 0.84 and a typical cruise of Mach 0.75 at heights up to when lightly loaded.Andrews 1966, p. 16.Blackman and Wright 2015, pp. 17–18. A drogue parachute was not necessary even operating from runways as short as .
The wing was mounted high on the fuselage and the location of the engines and main landing gear within the wing limited the volume available for fuel. The trailing edge of the wing had two-section with , and inboard of the ailerons were double-slotted flaps.Gunston and Gilchrist 1993, pp. 75–76. Direct electric motor were used to move the flaps and landing gear. The only hydraulically-operated equipment, the steering and brakes, was also powered by electric motors but driving hydraulic pumps instead of mechanical gearing.Gunston and Gilchrist 1993, p. 76.
Production aircraft were powered by four Avon 201 turbojet engines, with thrust. The engines also provided bleed air for the pressurization, ice protection, and air conditioning systems. The aircraft's DC electrical generators were also driven by the engines. Napier Spraymat electric heating were installed in the engine inlets to prevent ice formation and subsequent shedding possibly causing engine damage. The shape of the engine inlets were long rectangular slots in the first prototype, whereas production Valiants had oval or "spectacle" shaped inlets designed to pass greater airflow for the more powerful engines that were installed. The jet exhausts emerged from fairings above the trailing edge of the wings.
For required takeoff performance from short tropical dispersal bases,Gunston 1973, p. 50. a jettisonable RATO pack was developed for the Valiant. Trials were performed with two underwing de Havilland Sprite boosters; they were no longer needed when more powerful variants of the Avon engine became available. Also, there was an increased risk of accidents if one booster rocket failed on takeoff, resulting in asymmetric thrust.Blackman and Wright 2015, p. 20. Some Valiant engines had water injection, which increased takeoff thrust by about per engine.Darling 2012, p. 41.
The crew were in a pressurized compartment in the forward fuselage and consisted of a pilot, co-pilot, two navigators, and air signaller (later called an air electronics officer (AEO)).Blackman and Wright 2015, p. 28. Manufacture of this pressurized section was subcontracted to Saunders-Roe. The pilot and co-pilot were located side by side on an upper level, the remaining three crew members sat at stations lower in the cockpit, and faced to the rear.Gunston and Gilchrist 1993, pp. 74–75. The crew was reduced to five with the deleted requirement for defensive and , an operational philosophy proved by the De Havilland Mosquito bomber of World War II. The pilot and copilot were provided with Martin-Baker Mk.3 , while the rear crew had to bail out of the oval main entrance door on the port side of the fuselage.Turpin 2002, pp. 79–80. Safe escape using this exit was not considered likely.
The fuselage area behind the pressurised crew section and forward of the wing was used to house much of the avionics, and air conditioning equipment, and was sometimes called the "organ loft".Gunston and Gilchrist 1993, p. 75. The Valiant had twin-wheel nosegear and tandem-wheel main gear that retracted outwards into recesses in the underside of the wing. Each of the main gears were equipped with multipad anti-skid , and were telescopically linked so that a single drive motor could pull them up into the wing recesses. Most of the aircraft systems were electric, including the flaps and undercarriage.Darling 2012, p. 39. The brakes and steering gear were electrically powered, driving hydraulic pumps for actuation. The lower half of the aircraft nose contained the scanner for the H2S radar in a glass fiber radome; in addition, a visual bomb sight was located beneath the lower floor of the pressurised cockpit. The avionics bay was not accessible from the cockpit but could be accessed using an entrance at the base of the rear fuselage leading to an internal catwalk above the aft part of the bomb bay.Gunston and Gilchrist 1993, pp. 76–77.
The electrical systems used 112 volt direct current generators, one on each engine, for functions requiring large amounts of electrical power. A 28 V DC system was used for other uses including actuators that controlled the higher-voltage system functions. Backup power came from 24 V and 96 V batteries. 115 V alternating current was provided for the radar and the for the flight surfaces, flaps, air brakes and undercarriage. Flight 4 July 1958, p. 19.Turpin 2002, p. 78. It was decided during the design phase that as much of the aircraft would be electrically driven as was possible; the complete electrical system including high voltage generators and cabling, together with electric motors with mechanical drives, was lighter than the hydraulic equivalent consisting of pumps, tubing, actuators, fluid and storage tanks.
The flight controls of the Valiant (ailerons, elevator and rudder) consisted of two channels of power control with full manual backup; flying in manual was practised during training as it would be required if a complete electrical failure occurred during a flight. In "manual" the flight controls required considerable physical effort to operate.Blackman and Wright 2015, p. 18. The pilot's controls for elevators, ailerons and rudder had an artificial feel system, the pressure for which was provided from a ram-air intake.
A Smith Aerospace autopilot and instrument landing system (ILS) was installed along with various , such as the Marconi Company-built Green Satin doppler radar, Gee radio navigation, Automatic Direction Finder (ADF), VOR/Distance Measuring Equipment (DME), and . Provisions for additional equipment and sensors, such as side looking airborne radar, were also made.
The centre fuselage of the Valiant had a main backbone beam to support the weight of the two widely-set wing spars and five in the upper fuselage. The bomb bay was also in the lower half of the centre fuselage. Flight 4 July 1958, p. 18. The aft fuselage used a monocoque structure, being lighter than the centre fuselage; the Boulton-Paul-produced electro-hydraulic power units for the ailerons, elevators, and rudder were contained within this space. The tail, which was attached to the rear fuselage was Cone rather than swept back, the horizontal tailplane was mounted well up the vertical fin to keep it clear of the engines' exhaust. The tailcone contained an ARI 5800 Orange Putter tail warning radar.
The main structural components, spars and beams of the Valiant had been constructed from a zinc/magnesium/copper aluminium alloy called DTD683 in the UK. Flight 14 December 1951, p. 756. Flight 17 July 1953, p. 91. The Valiant had been designed with a 'Safe-life design' strategy;Brookes 2012, p. 83. this combination of 'Safe-Life' and DTD683 came to be viewed as a severe mistake. In 1956, a publication within the Journal of the Institute of Metals The Journal of the Institute of Metals (JIM), Vol. 86, No. 1790, 1957–1958. condemned the material DTD683 as being unstable and capable of catastrophic failure when stressing the airframe close to its design limits. The "Safe-Life" design strategy was dismissed by a Lockheed engineer in a talk given to the Royal Aeronautical Society in 1956, because it did not guarantee safety from catastrophic failure. Flight 6 April 1956, p. 394.
The Valiant B.1 could carry a nuclear weapon or up to 21 conventional in its bomb bay. It was designed for the early Nuclear fission-based nuclear weapons and also the newer and larger thermonuclear . A "clean" Valiant (one without underwing tanks) could climb straight to 50,000 ft after takeoff unless it had heavy stores in the large bomb bay.
In the aerial reconnaissance role, a camera crate would be installed in the bomb bay, along with a pair of cameras set into the fuselage and larger rear fuel tanks to extend the aircraft's endurance.Blackman and Wright 2015, p. 19. Large external fuel tanks under each wing with a capacity of , could be used to extend range; an auxiliary fuel tank could also be installed in the forward area of the bomb bay; the external wing tanks were fitted as standard on Valiants that were operated as aerial refuelling tankers. For receiving fuel, a fixed refuelling probe was fitted onto the aircraft's nose, this was connected to the fuel tanks via a pipe running along the outside of the canopy to avoid penetrating the pressure cabin.Gunston and Gilchrist 1993, p. 79.
According to Gunston and Gilchrist, the Valiant had performed "extremely well" during the annual bombing competition hosted by American Strategic Air Command (SAC). American interest in the Valiant resulted in a visit to Vickers by USAF generals Hoyt Vandenberg, Johnson and Curtis LeMay. Vickers test-pilot Brian Trubshaw believed that George Edwards was put under some pressure to build the Boeing B-47 under license. The only result from the visit was Le May's insistence that the Valiant pilot side-by-side seating be incorporated in the B-52 instead of the tandem arrangement in the B-47 and prototype B-52.Brian Trubshaw Test Pilot, Brian Trubshaw and Sally Edmondson, Sutton Publishing Limited 1999, , p.35
On 11 October 1956, a Valiant B.1 (WZ366) of No. 49 Squadron piloted by Edwin Flavell was the first British aircraft to drop an atomic bomb when it performed a test drop of a down-rated Blue Danube weapon on Maralinga, South Australia.Mason 1994, p. 378. This occurred as part of the Operation Buffalo nuclear tests in that area. Windscreen blinds were fitted in advance of the test to protect the crew from the intense flash of light from the nuclear detonation. Following the landing of the aircraft after deploying the weapon, WZ366 was assessed for potential damage and for radioactive contamination.Blackman and Wright 2015, pp. 33–36.
On 15 May 1957, a Valiant B(K).1 (XD818) piloted by Kenneth Hubbard dropped the first British hydrogen bomb, the Short Granite, over the Pacific as part of Operation Grapple. No 49 Squadron was selected to perform the live weapon drop, and were equipped with specially-modified Valiants to conform with the scientific requirements of the tests and other precautionary measures to protect against heat and radiation.Hubbard and Simmons 2008, pp. 61, 68. However, the measured yield was less than a third of the maximum expected although achieving a thermonuclear explosion.
On 8 November 1957 a British hydrogen bomb detonated with its planned yield in the Grapple X test.Hubbard and Simmons 2008, p. 157. The Grapple series of tests continued into 1958, and in April 1958 the Grapple Y bomb exploded with ten times the yield of the original "Short Granite".Hubbard and Simmons 2008, p. 167. Testing was finally terminated in November 1958, when the British government decided it would perform no more air-delivered nuclear tests.
Originally the bombing role was to have been carried out at high altitude, but following the shooting down in 1960 of the Lockheed U-2 flown by Gary Powers by an early Soviet SA-2 Guideline missile, the SAM threat caused bomber squadrons to train for low-level attack as a means of avoiding radar detection when flying within hostile airspace. They were repainted in grey/green camouflage with normal markings, replacing their anti-flash white scheme. By 1963, four Valiant squadrons (49, 148, 207 and 214) had been assigned to SACEUR in the low-level tactical bombing role. By this point, there had been a noticeable decline in flying rates for the type.
In October and November 1956 the Valiant was the first of the V-bombers to see combat, during the Anglo-French-Israeli Suez campaign. During Operation Musketeer, the British military operation in what became known as the Suez Crisis, Valiants operating from the airfield at Luqa on Malta dropped conventional bombs on targets inside Egypt. Egyptian military airfields were the principal target; other targets included communications such as and transport hubs.Bowman 2016, p. 158 On the first night of the operation, six Valiants were dispatched to bomb Cairo West Air Base (which was aborted in flight due to potential risk to US personnel in the vicinity) while six more attacked Almaza Air Base and a further five bombed Kibrit Air Base and Huckstep Barracks.Blackman and Wright 2015, p. 42.Darling 2012, p. 42.
Although the Egyptians did not oppose the attacks and there were no Valiant combat losses, the results of the raids were reported as disappointing. Although the Valiants dropped a total of of bombs, only three of the seven airfields attacked were seriously damaged. The Egyptian Air Force had been effectively destroyed in a wider series of multinational attacks of which the Valiant bombing missions had been a part.Bowman 2016, pp. 158, 161. It was the last time RAF V-bombers flew a live combat mission until Avro Vulcans bombed Port Stanley airfield in the Falkland Islands during the Falklands War in 1982.McClelland, pp.175–178.
Long-range demonstration flights were made with in-flight refuelling by other Valiant tankers that had been positioned at airfields along the route. In 1960, a Valiant bomber flew non-stop from Marham in the UK to Singapore and in 1961 a Vulcan flew non-stop from the UK to Australia.Hubbard and Simmons 2008, p. 26. The two tanker squadrons regularly made long range flights. These included non-stop flights from the UK to Nairobi, RAF Gan and Singapore.Brookes 1982, pp. 141–142 Other aircraft refuelled by Valiants at this time included Victor and Vulcan bombers, English Electric Lightning fighters, and de Havilland Sea Vixen and Supermarine Scimitar fighters of the Royal Navy.Wynn 1994, p. 168.
Valiants of No. 543 Squadron at RAF Wyton were modified to serve in the photographic reconnaissance role. In one notable operation in 1965, Valiants of No. 543 Squadron photographed around of Rhodesia across an 11-week period.
Later the RAE ran a similar series of tests that more closely resembled actual operational conditions including low level and taxiing; the corresponding report published in 1958 produced data that could be used to get a better grasp on which flight conditions produced the most damage, and enable a better projection of the future life span for the type. "Fatigue Loadings in Flight-Loads in the Nose Undercarriage and Wing of a Valiant." E.W. Wells, ARC C.P. No. 521.
In May 1957 Flight reported an "incident at Boscombe Down, when the wing rear spar cracked after a rocket-assisted takeoff at overload weight (the reason for the rocket-assistance)" Flight 17 May 1957, p. 651 This aircraft was the second prototype WB 215 and had not been modified with the production fix for the known weakness in the rear spar;Properly to Test Book One "The Early Years",Noble 2003,,p.96 the aircraft was subsequently broken up for wing fatigue testing after it had flown 489 hours.Morgan p. 44 & p. 89.
After years of front-line service, in July 1964, a cracked spar was found in one of the three Valiants (either WZ394 – Wynne, or WZ389 – Morgan) on Operation Pontifex.Wynn p. 469. This was followed on 6 August by a failure of the starboard wing rear spar at 30,000 ft,Brookes, Victor Units of the Cold War, p. 67. in WP217, an OCU aircraft from Gaydon captained by Flight Lieutenant "Taffy" Foreman. The aircraft landed back at Gaydon but without flap deployment because damage to the starboard rear spar caused the flap rollers to come out of their guides so that the flap would not lower on that side. Later inspection of the aircraft also showed the fuselage skin below the starboard inner plane had buckled, popping the rivets; the engine door had cracked and the rivets had been pulled and the skin buckled on the top surface of the mainplane between the two engines.Darling 2012, pp. 39–40. Both of these aircraft were PR variants.Morgan, App 2, Individual Valiant Histories pp. 89–94.
Inspections of the entire fleet showed that the wing spars were suffering from fatigue at between 35% and 75% of the assessed safe fatigue life, probably due to low level turbulence.Darling 2012, p. 40. After this inspection, the aircraft were divided into three categories, Cat A aircraft continuing to fly, Cat B to fly to a repair base, and Cat C requiring repair before flying again. The tanker squadrons had the highest proportion of Cat A aircraft because their role had been mainly at high level. This also caused the methods of assessing fatigue lives to be reviewed.Wynn 1996, p. 465. By the time the type was scrapped, only about 50 aircraft were still in service; the rest had been slowly accumulating at various RAF Maintenance Units designated as "Non effective Aircraft".Morgan App2, pp. 89–94.
Initially there was no question of retiring the type, or even a majority of affected aircraft. Repairs were actively taking place at Valiant bases such as Marham using working parties from Vickers plus RAF technicians from the base. In January 1965, the Wilson government with Denis Healey as Secretary of State for Defence decided that the expense of the repairs could not be justified, given the short operational life left to the Valiant, and the fleet was permanently grounded as of 26 January 1965. "Valiants to be Scrapped." Glasgow Herald, 27 January 1965. The QRA alert that had been in place for SACEUR was maintained until the final grounding.Wynn 1996, pp. 464–471, 500. When asked to make a statement regarding the Valiant's scrapping in the House of Commons, Denis Healey stated that it "was not in any way connected with low-level flying" and that the "last Government took the decision to continue operating the Valiant force for another four years after its planned fatigue life was complete".
Aviation author Barry Jones commented in his book that: "A question has to be asked. For two years before the demise of the Valiant, Handley Page at Radlett had 100 Hastings go through their shops. They were completely dismantled and rebuilt, having DTD683 components removed and replaced by new alloy sections. What was so special about the Hastings and why was the Valiant not treated similarly? Perhaps we will know one day – but I doubt it.""V-Bombers" Barry Jones p. 117. A Flight report about the scrapping states "Fatigue affected all Valiants ... not only those that had been used for some low flying".
On 9 December 1964, the last Valiant tanker sortie in XD812 of 214 Squadron was refuelling Lightning aircraft over the North Sea and was recalled to land back at Marham before the scheduled exercise was completed. On the same day, the last Valiant bomber sortie was carried out by XD818.
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