Bernard 260 • wp.archivoaereo.com

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Initial Development of the Bernard 260

In late 1931, designers at Société des Avions Bernard embarked on the creation of a new fighter aircraft, building upon the Bernard 74. This new project, designated Bernard 260, was ready by early the following year.

The Bernard 260 was a single-seat, all-metal low-wing monoplane, powered by a 690 hp Hispano-Suiza 12Xbrs engine. Its maiden flight occurred in September 1932, marking the beginning of its evaluation phase.

Competitive Trials for the French Air Force

Almost immediately after its first flight, the aircraft was handed over to the military for competitive trials at the Villacoublay airfield. The Bernard 260 participated in a competition for a light fighter for the French Air Force, competing against about a dozen aircraft from various firms.

Ultimately, the Dewoitine D.500 emerged as the winner of this demanding competition. Despite not being selected, the Bernard 260 proved to be a valuable platform for further research.

Legacy and Adaptation

Subsequently, the Avions Bernard aircraft was utilized in the development work for creating a float fighter. This adaptation aimed to explore new capabilities for French naval aviation, showcasing the versatility of its design.

Technical Specifications

Modification	Bernard 260
Wingspan, m	11.30
Length, m	7.80
Wing area, m2	18.20
Empty weight	1357
Normal takeoff weight	1800
Engine type	1 Piston engine Hispano-Suiza 12Xbrs
Power, hp	1 x 690
Maximum speed, km/h	376
Cruising speed, km/h	335
Service ceiling, m	10200
Crew	1 crew member
Armament	Two 7.5-mm Darne machine guns