My thanks to Roger Dunn and the MOD for supplying these images.Wikipedia for text.
Design Company: Vickers-Armstrongs Ltd, Weybridge & Hurn First Flight: 30 June 1947 Valetta Prototype: 1 - Vickers-Armstrongs Ltd Valetta C.1: 211 - Vickers-Armstrongs Ltd Valetta C.2: 11 - Vickers-Armstrongs Ltd Valetta T.3: 40 - Vickers-Armstrongs Ltd Type Specification Applies to: Vickers Valetta C.1 Type: Twin engined military transport Wing: Cantilever mid wing monoplane. All metal structure Fuselage: All metal oval section monocoque structure Tail Unit: Cantilever monoplane type. All metal structure Landing Gear: Retractable two wheel type. Each main wheel retracts rearwards into engine nacelle. Tail wheel retracts rearwards into fuselage Power Plant: Two 1,975 hp Bristol Hercules 230 nine cylinder air cooled radial engines driving De Havilland or Rotol four blade constant speed feathering airscrews 13 ft 3 in diameter Accommodation: Crew of four comprising two pilots, navigator and radio operator Dimensions Span: 89 ft 3 in Length: 62 ft 11 in Height: 19 ft 7 in Wing Area: 882 sq ft Weights Empty: 24,980 lb Gross: 36,500 lb Performance Max Speed: 258 mph at 10,000 ft Initial Rate of Climb: 1,275 ft/min Service Ceiling: 21,500 ft Range: 1,460 miles |
Some aircraft may appear identical but there are differences which will not be discernible from the image.
(Be patient with loading)
![]() |
267 Squadron |
![]() |
Vickers Valetta
|
(Be patient with loading)