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Burnelli UB-14

UB-14
Cunliffe-Owen OA-1 airliner in Egypt 1942.jpg
Role Civil transport
Manufacturer Burnelli
Designer Vincent Burnelli
First flight 1934
Number built 3
Developed into Burnelli CBY-3

The Burnelli UB-14 was a 1930s American prototype lifting-fuselage airliner designed and built by Vincent Burnelli.

Following on from his earlier designs Vincent Burnelli designed a commercial transport version using the lifting-fuselage concept. Burnelli's designs were based on the idea that an airfoil-section fuselage would contribute to the lift generated. The Burnelli UB-14 first flew in 1934, the airfoil-section fuselage was the centre-section of the wing. The aircraft had twin tailbooms and a widespan tailplane and elevator fitted with twin fins and rudders. The UB-14 had retractable landing gear and was powered by two Pratt & Whitney radial engines. An enclosed cockpit for the crew of two was located on the centre wing's upper surface. The cabin held 14 to 18 passengers.

The first prototype, UB-14, was destroyed in a 1935 accident attributed to faulty maintenance on the aileron control system. Burnelli then designed and built an improved version, the UB-14B. A modified version of the UB-14B design was built under licence in the United Kingdom by Cunliffe-Owen Aircraft, powered by two Bristol Perseus XIVC radials as the Cunliffe-Owen OA-1. A contemporary photo shows the mockup of the original UB-14B, to be built by Scottish Aviation before bankruptcy. This design was to have had streamline inline engines. The OA-1 used radial engines.

In September 1936, Burnelli applied to the CAA for approval to fly a transatlantic flight with Clyde Edward Pangborn as the selected pilot.


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