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Data from Vickers Aircraft Co Ltd General characteristics Crew: 1 Capacity: 2 Length: 24 ft 7 in (7.5 m) Wingspan: 30 ft 10 in (9.40 m) Height: 7 ft 6 in (2.29 m) Wing area: 149.3 sq ft (13.87 m 2) Empty weight: 928 lb (421 kg) useful load 650 lbs Gross weight: 1,850 lb (839 kg) Fuel capacity: 60 U.S. gallons (230 L; 50 imp gal) Powerplant: 1 × Rotax 915iS horizontally opposed turbocharged ...
Vickers Aircraft Company's first aircraft, a two-seat amphibious seaplane, is called The Wave. [5] The Wave has some unique features unavailable in other similar aircraft, [6] such as a bow thruster and substantially higher horsepower engine. [7] [8] [9]
Pages in category "Vickers aircraft" The following 86 pages are in this category, out of 86 total. This list may not reflect recent changes. 0–9. 23-class airship;
Aircraft Photograph Build date First flight Last flight Operator Location Status Notes Ref. XD818 1956 September 4th, 1956 January 1965 Royal Air Force: RAF Museum Cosford, RAF Cosford, Shropshire, England: On static display [1] [2] [3] XD816 1956 1956 1968 Royal Air Force: Brooklands Museum Weybridge, Surrey, England: On static display Cockpit ...
This was owned by Vickers, English Electric and Bristol (holding 40%, 40% and 20% respectively). BAC in turn owned 70% of Hunting. The Supermarine operation was closed in 1963 and the Vickers name for aircraft was dropped in 1965.
This is a list of aircraft in alphabetical order beginning with 'V'. ... (Vickers Aircraft Company) Vickers Aircraft Wave; Vickers (Vickers plc) see: Vickers-Armstrongs;
Between 1923 and 1944, Canadian Vickers produced over 400 aircraft, some of which were original Vickers' designs while the remainder were other manufacturers' designs built under license. This Canadian Vickers OA-10A operated in several countries postwar as a utility transport, including Hong Kong, Sweden and Kenya Canadian Vickers PBV-1A Canso ...
The Vickers-Wibault construction method was based on the patents of Michel Wibault, who began working with Vickers in 1922. [1] It was a way of producing an all-metal aircraft with an airframe built up from simple, non-machined metal shapes, covered with very thin e.g. 0.016 in (0.4 mm) corrugated light alloy sheets.