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Vickers Valetta

From Alfawiki
Vickers-Armstrongs Ltd
Company typePrivate company
IndustryAerospace, Defence
Headquarters
United Kingdom
ProductsMilitary transport aircraft, including Vickers Valetta, Vickers VC.1 Viking, Vickers Varsity


The Vickers Valetta is a twin-engine military transport aircraft engineered and manufactured by the British firm Vickers-Armstrongs Ltd. It evolved from the compact civilian airliner, the Vickers VC.1 Viking, featuring an all-metal mid-wing monoplane design equipped with a conventional tailwheel undercarriage.

Development of the Valetta began shortly after World War II, driven by the Royal Air Force's (RAF) requirement for a versatile military transport derived from the Viking. The aircraft was expected to fulfill multiple roles rapidly, including troop transportation, medical evacuation, cargo carriage, glider towing, and paratroop deployment. To support these diverse functions, the interior fittings were designed for quick removal and replacement with alternative configurations. Key modifications from the Viking included installation of more powerful Bristol Hercules 230 radial engines, reinforcement of the cabin floor, and strengthening of the landing gear.

Following its maiden flight on 30 June 1947, the Valetta entered RAF service in 1948. It soon became integral to Transport Command operations and took part in various British military engagements during the 1950s and 1960s such as the Suez Crisis, Aden conflict, and Malayan Emergency. The platform was further adapted into several variants including VIP transport and multiple trainer versions. Most notably, it served as the foundation for the Vickers Varsity, a specialised military training aircraft.

Background

The Valetta’s genesis is closely linked to its predecessor, the Vickers VC.1 Viking—a civilian airliner itself developed from the Second World War-era Vickers Wellington medium bomber. Towards the end of the Viking’s development phase, it underwent thorough assessments by RAF officials. Interest grew within RAF circles for a military transport variant to replace ageing wartime transports within RAF Transport Command.

Responding to this demand, the Air Ministry formalised a specification—C.9/46—targeted specifically at Vickers’ design. Aviation historian C. F. Andrews noted that this requirement was notably progressive for its time, mandating rapid role conversion capabilities including troop carrying, air ambulance duties, freight hauling, glider towing, and air-dropping of paratroopers and supplies.

Into flight

The initial Valetta prototype, originally constructed as a standard Viking (c/n 158), reached completion in early 1947. On 30 June 1947, this prototype conducted the aircraft's inaugural flight at Brooklands, with Vicker's test pilot Joseph "Mutt" Summers at the controls.

Despite being named after Malta's capital city Valletta, the aircraft's designation uses a single "l" in its spelling. Both the Viking and Valetta served as foundational designs for the development of the Vickers Varsity. While the Varsity bore similarities to its predecessors, it was slightly larger, featured a tricycle undercarriage configuration, and included a distinctive under-fuselage pannier designed to house a bomb-aimer and carry up to 24 practice bombs.

Design

The Vickers Valetta was developed as a twin-engine military transport aircraft. Key distinctions from its Viking predecessor included the installation of more powerful engines, a reinforced cabin floor, and the addition of large, robust double doors on the fuselage’s side to facilitate cargo loading and unloading. The need for enhanced engine power arose primarily due to an approximate 2,000-pound increase in maximum takeoff weight compared to the Viking. The Valetta was powered by two Bristol Hercules 230 radial engines, each delivering up to 2,000 horsepower.

Designed to accommodate a wide range of military cargoes—including bulky items—the interior floor was engineered to withstand concentrated loads of up to 1,500 pounds per point. The floor was also equipped with numerous tie-down points for securing freight. Many interior components were made quickly removable to allow rapid role changes; these included various seating arrangements, a loading winch, vehicle ramps, floor rollers, equipment for glider towing, extra fuel tanks, and soundproofing along the sidewalls. In troop transport configuration, the Valetta could carry as many as 34 fully equipped soldiers. When configured as an air ambulance, it could transport 20 stretcher patients accompanied by two medical attendants. In its paratroop setup, it accommodated up to 20 paratroopers plus nine supply containers weighing 350 pounds each that could be air-dropped.

Externally, the Valetta featured several adaptations for payload handling. Twin racks beneath the center fuselage allowed carriage of supply containers. A pyramid-shaped structure at the rear fuselage served both as an attachment point and release mechanism for towing gliders. For missions requiring extended range, optional flexible bag tanks could be added. To cope with heavier payloads anticipated from Viking operations and to endure rough field landings more effectively, the undercarriage was significantly strengthened.

Operational history

The Valetta C.1 was introduced into RAF service in 1948. Its widespread deployment swiftly phased out the wartime Douglas Dakota aircraft within RAF Transport Command, including numerous transport units based throughout the Middle East and Far East regions. The Valetta was actively employed in conflict zones, notably conducting multiple parachute operations over Egypt during the 1956 Suez Crisis. Throughout the 1950s and 1960s, this aircraft frequently fulfilled transport duties supporting various British military campaigns, such as those during the Malayan Emergency and in Aden.

File:Vickers 664 Valetta T.3 WG266 RAFC BLA 09.56.jpg
Vickers Valetta T.3 assigned to the RAF College at Blackbushe Airport in September 1956. Notice the cabin-top astrodomes and antennae used for navigation training
File:Vickers Valetta T.4 WJ485 2 ANS MStG 14.09.63 edited-3.jpg
Valetta T.4 from No.2 Air Navigation School featuring an extended radar nose

Although most Valettas were produced to the C.1 configuration, several specialized variants were also introduced. The Valetta C.2 served as a dedicated VIP transport, maintaining similar performance characteristics but with enhanced range capabilities.

Designed for navigational instruction, the Valetta T.3 was operated by the RAF College at RAF Cranwell as well as No.1 and No.2 Air Navigation Schools. This variant is identifiable by multiple astrodomes installed along the upper fuselage. Deliveries of 40 T.3 aircraft commenced in August 1951, concluding with WJ487 in September 1952. Subsequently, 18 of these were converted into the T.4 model, which incorporated a larger nose housing a radar system, thus enabling training for aircraft interception radar operations.

Certain Valettas underwent modifications as part of experimental programs conducted by Vickers. Various alternative landing gear configurations were tested; however, these changes reportedly had minimal impact on ground handling compared to the standard setup.

Variants

  • Valetta C.1 – designed for transport duties, with a total of 211 units produced
  • Valetta C.2 – configured for VIP transport, with 11 aircraft manufactured
  • Valetta T.3 – utilized as an aircrew trainer, 40 examples completed
  • Valetta T.4 – modified from the T.3 variant, equipped with a nose-mounted radar system

Operators

Template:UK
Squadron Service Period Start Service Period End Base Locations Additional Information
No. 30 Squadron RAF November 1950 May 1957 RAF Abingdon
RAF Benson
RAF Dishforth
[1]
No. 48 Squadron RAF June 1950
May 1951
September 1950
December 1957
RAF Changi [2]
No. 52 Squadron RAF June 1951 April 1966 RAF Changi
RAF Kuala Lumpur
RAF Butterworth
[2]
No. 70 Squadron RAF January 1950 January 1956 RAF Kabrit
RAF Fayid
RAF Nicosia
[3]
No. 78 Squadron RAF April 1950 September 1954 RAF Kabrit
RAF Fayid
Disbanded[4]
No. 84 Squadron RAF February 1953 December 1956 RAF Fayid
RAF Abu Sueir
RAF Nicosia
Disbanded[5]
No. 84 Squadron RAF December 1956 August 1960 RAF Khormaksar Reformed[5]
No. 110 Squadron RAF October 1951 December 1957 RAF Changi [6]
No. 114 Squadron RAF September 1949 December 1957 RAF Kabrit
RAF Fayid
RAF Abu Sueir
RAF Nicosia
Disbanded[7]
No. 115 Squadron RAF August 1963 May 1964 RAF Tangmere
RAF Watton
[7]
No. 204 Squadron RAF May 1949 February 1953 RAF Kabrit
RAF Fayid
Disbanded[8]
No. 216 Squadron RAF November 1949 November 1955 RAF Kabrit
RAF Fayid
[9]
No. 233 Squadron RAF September 1960 January 1964 RAF Khormaksar Reformed and subsequently disbanded[10]
No. 622 Squadron RAF November 1950 September 1953 RAF Blackbushe Reformed before disbandment[11]
No. 683 Squadron RAF November 1950 November 1953 RAF Fayid
RAF Kabrit
RAF Eastleigh
RAF Khormaksar
RAF Habbaniya
[12]
Royal Air Force College Cranwell     RAF Cranwell [13]
No. 1 Air Navigation School RAF March 1957 August 1970 RAF Topcliffe
RAF Stradishall
[14]
No. 2 Air Navigation School RAF     RAF Thorney Island [14]
No. 3 Air Navigation School RAF March 1952 April 1954 RAF Bishops Court [14]
No.5 Air Navigation School RAF March1951 November1952 RAFLindholme [14]
No.6 Air Navigation School RAF February1952 December1953 RAFLichfield [14]
No.228 Operational Conversion Unit RAF October1956 1961 RAFNort hLuffenham
RAFLeeming
[15]
Overseas Ferry Unit RAF     RFA bingdon [16]


Accidents and incidents

  • On 18 February 1951, an RAF Valetta was compelled to perform a belly landing near Stockholm-Bromma Airport due to engine failure and communication issues. The situation was further aggravated by airframe icing. Among the 22 passengers and crew, one fatality occurred. The aircraft was completely destroyed.Template:Fix/category[citation needed]
  • On 15 January 1953, Valetta C.1 VX562 was involved in a mid-air collision over the Mediterranean Sea with an RAF Lancaster, resulting in the deaths of all 19 individuals aboard the Valetta and seven crew members on the Lancaster.[17]
  • VX490 vanished on 11 November 1953 during an air test flight after departing RAF Changi. All seven occupants perished, with the aircraft believed to have disintegrated in a thunderstorm.Template:Fix/category[citation needed]
  • On 6 January 1954, Valetta T.3 WJ474 crashed close to Aldbury, Hertfordshire while attempting takeoff in adverse weather conditions from RAF Bovingdon. The aircraft was transporting a rugby team; seventeen people lost their lives, with one survivor.[18][19]
  • Valetta C.1 WJ494, arriving from Hong Kong, crashed approximately 2.4 km (1.5 mi) from Singapore's Changi RAF base on 21 February 1954 during a single-engine approach. It was reported that the pilot mistakenly feathered the wrong engine while approaching the runway. The aircraft lost altitude, collided with trees, and caught fire; three of the twelve occupants died.[20]
  • On 17 April 1957, Valetta C.1 VW832 crashed at Queria, Jordan, five minutes after departing from King Hussein International Airport. The left wing detached following turbulence encounter, causing the crash that killed all 26 people onboard.[21]
  • RAF Valetta VX491 'Y' crashed in dense jungle near Tanjong Malim, Malaya on 22 August 1957. Three RAF crew members died while four servicemen from 55 Coy RASC AD survived and were rescued. Engine failure is considered a possible cause.Template:Fix/category[citation needed]

Aircraft on display

File:Flixton Air Museum - geograph.org.uk - 371807.jpg
A Valetta C.2 preserved at the Norfolk and Suffolk Aviation Museum

Specifications (Vickers Valetta C.1)

Template:Aircraft specs

Notable appearances in media

The Valetta T3 is prominently featured in an extended sequence of the 1957 movie High Flight, where it serves as an airborne navigation training classroom at RAF College Cranwell.

See also

Template:Aircontent

Citations

  1. ↑ Jefford 2001, p. 38.
  2. ↑ 2.0 2.1 Jefford 2001, p. 44.
  3. ↑ Jefford 2001, p. 49.
  4. ↑ Jefford 2001, p. 51.
  5. ↑ 5.0 5.1 Jefford 2001, p. 53.
  6. ↑ Jefford 2001, p. 58.
  7. ↑ 7.0 7.1 Jefford 2001, p. 60.
  8. ↑ Jefford 2001, p. 71.
  9. ↑ Jefford 2001, p. 74.
  10. ↑ Jefford 2001, p. 77.
  11. ↑ Jefford 2001, p. 102.
  12. ↑ Jefford 2001, p. 105.
  13. ↑ Sturtivant & Hamlin 2007, p. 227.
  14. ↑ 14.0 14.1 14.2 14.3 14.4 Sturtivant & Hamlin 2007, p. 49.
  15. ↑ Sturtivant & Hamlin 2007, p. 197.
  16. ↑ Sturtivant & Hamlin 2007, p. 208.
  17. ↑ "Accident Description: Valetta C1." aviation-safety.net.
  18. ↑ "Accident Description: Valetta T3." aviation-safety.net.
  19. ↑ Service Aviation Flight 15 January 1954
  20. ↑ "ASN Aircraft accident Vickers Valetta C.1 WJ494 Singapore-Changi RAF Station" aviation-safety.net.
  21. ↑ "ASN Aircraft accident Vickers Valetta C.1 VW832 Queria" aviation-safety.net.
  22. ↑ Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
  23. ↑ Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
  24. ↑ Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).

Bibliography

  • Andrews, C.F. Vickers Aircraft Since 1908. London: Putnam, 1969.
  • Andrews, C.F. and E.B. Morgan. Vickers Aircraft since 1908. London: Putnam, 1988. ISBN 0-85177-815-1.
  • Bridgman, Leonard. Jane's All the World's Aircraft 1951–52. London: Sampson Low, Marston & Company, Ltd, 1951.
  • Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
  • Martin, Bernard. The Viking, Valetta and Varsity. Air-Britain (Historians) Ltd. 1975. ISBN 0-85130-038-3.
  • Lua error in Module:Citation/CS1/Configuration at line 2123: attempt to index field '?' (a nil value).
  • Thetford, Owen. Aircraft of the Royal Air Force 1918-57. London: Putnam, 1st edition, 1957.

External links

Template:Vickers aircraft Template:ADF aircraft designations