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Caudron C.520 Simoun VI

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Caudron C.520 Simoun VI

In 1934, at the Paris Air Show, the Société des Avions Caudron company presented the Caudron C.520 Simoun VI, a light multi-purpose aircraft. It was a four-seater cantilever low-wing monoplane, equipped with a 170 hp six-cylinder Renault Bengali 6Q-06 (6Pfi) engine.

Innovative Design Features

The aircraft, which was developed based on the C.500, featured separate comfortable passenger seats, three large portholes on each side, and a very practical windshield.

The C.520 boasted an all-metal construction, which provided it with additional strength, thereby making its operation very reliable and practical. An increased fuel capacity allowed the aircraft to undertake longer flights.

A Prototype’s Enduring Legacy

The Caudron C.520 Simoun VI did not enter series production, remaining as a single example (F-ANCC). Nevertheless, its further refinement led to the development of an entire successful family of aircraft, the Caudron C.630 Simoun.

Technical Specifications

Modification C.520
Wingspan, m 10.40
Aircraft length, m 8.66
Wing area, m2 16.00
Empty weight 650
Maximum takeoff weight 1230
Engine type 1 Piston engine Renault Bengali 6Q-06
Power, hp 1 x 170
Maximum speed, km/h 300
Cruising speed, km/h 270
Practical range, km 1350
Practical ceiling, m 6000
Crew, crew members 1
Payload up to 3 passengers

Image and diagram gallery of the Caudron C.520 Simoun VI

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La información presentada en esta ficha técnica ha sido compilada a partir de manuales de vuelo desclasificados, archivos históricos y bibliografía especializada. Aunque nos esforzamos por mantener la máxima precisión, algunos datos de rendimiento pueden variar según la variante específica o las condiciones operativas.

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