Bernard 207T

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The Bernard 207T was the final representative of the large Bernard 200 family of aircraft, developed and built by the French company Societe des Avions Bernard. This model was conceived as a light, multi-purpose aircraft, marking the culmination of a series of aviation designs.

Table of Contents

First Flight and Technical Specifications

The prototype made its maiden flight on July 20, 1933. It was a four-seater, cantilever high-wing monoplane. Power was supplied by a four-cylinder De Havilland Gipsy Major I engine, delivering 120 hp.

Development and Performance

Two Bernard 201T aircraft (F-AMOS and F-AMGS) were later converted to this improved variant. The Bernard 207T boasted a wingspan of 11.96 m, a length of 7.70 m, and a height of 2.10 m. Its empty weight was 707 kg, with a normal takeoff weight of 1030 kg, and it could reach a maximum speed of 195 km/h.

Technical Specifications

Modification	Bernard 207T
Wingspan, m	11. 96
Length, m	7. 70
Height, m	2.10
Wing area, m2	17. 20
Empty weight	707
Normal takeoff weight	1030
Engine type	1 Piston engine De Havilland Gipsy Major I
Power, hp	1 x 120
Maximum speed, km/h	195
Crew	4

Image and diagram gallery of the Bernard 207T

France

ArchivoAéreo Editorial Team

A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.

Sources & Accuracy

The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.

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