Vickers Type 253 K2771 '6'
Vickers Type 253 K2771 '6' taxying at the RAF Pageant at Hendon.
The Vickers Aviation Type 253 was a single engine, two seat biplane was designed by Barnes Wallis and Rex Pierson, to meet the requirements of Specification G.4/31 which called for a general-purpose bombing and torpedo aircraft to replace the Westland Wapati.
It was developed in parallel with a private-venture monoplane prototype, which later entered production as the Vickers Wellesley, described separately on its own web page.
The Type 423 was powered by a Bristol Pegasus engine and used a geodetic structure for the rear fuselage, drawing on the experience that Barnes Wallis had gained in the construction of airships – notably the Vickers-built R-100.
Vickers Type 253 internal structure
The Vickers Type 253 was Barnes Wallis' first aircraft to use a geodetic fuselage structure.
A geodesic is the shortest line between two points on a curved surface and Wallis identified this structural approach as providing efficient load distribution in a structure whilst also introducing redundant load paths to create a fail-safe and damage tolerant structure. The aim was to achieve a lattice-like structure that required no underlying secondary structure to give it strength.
In the Vickers Type 253, this system was partially introduced in the fuselage structure on the private-venture Vickers G.4/31 monoplane, developed by Vickers in parallel, adopting a full geodetic structure for both wings and fuselage.
Vickers Type 253 K2771 carrying torpedo
Vickers Type 253 K2771 photographed at Brooklands carrying a dummy torpedo.
The Vickers Type 253 (K2771) made its first flight at Brooklands on 16th August 1934, with Matt Summers at the controls, and powered by a 635 ho Bristol Pegasus IIM3 engine. In early 1935, this engine was replaced with a Bristol Pegasus IIIM3.
The Vickers Type 423 was the subject of comparative trials with the G.4/31 monoplane prototype at  the Aeroplane and Armament Experimental Establishment (A&AEE), Martlesham Heath and unfortunately, the G.4/31 demonstrated the clear advantage of the monoplane.  With its fully-geodetic structure, the monoplane had a lighter empty weight and had superior performance at higher weights than the Type 423 thereby delivering better payload and range characteristics.
As a result, further development of the Vickers Type 253 was abandoned, although the sole example (K2771) continued to give valuable service to the Bristol Engine Company as a flying test-bed.
Ultimately, the airframe was donated to 385 Sqn (Coulsdon & Purley) of the Air Training Corps where its ultimate fate is unknown.

Variants & Numbers

One aircraft only (K2771)



Powerplant One 635 hp Bristol Pegasus IIM3 engine
Span 52 ft 7 in
Maximum Weight 8,350 lb
Capacity and armament Pilot and observer; provision for the carriage of up to 8 bombs under the wings and a torpedo between the undercarriage legs. Armament two Lewis machine guns – one forward firing and one fired from the observer position.
Maximum Speed 161 mph at 4,500 ft




Other information

12 Default Profile Image
BAE Systems
The information shown is based on that available at the time of the content creation. If you have any additions or corrections then please contact us via email - All images BAE Systems / Ron Smith copyright unless otherwise shown.