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Caudron C.561

Posted on June 23, 2026 By

In 1936, Société des Avions Caudron built the C.561 racing aircraft. It represented a unique blend, incorporating the fuselage of the C.461 and the powerplant of the C.560, resulting in a single-seat, low-wing monoplane with a distinct construction.

Table of Contents

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    • Design and Technical Specifications
    • The Coupe Deutch Challenge and its Fate
    • Technical Specifications
  • Image and diagram gallery of the Caudron C.561
    • How to cite this article:

Design and Technical Specifications

The C.561 was equipped with a Renault 446 engine, delivering 450 hp. Its design, combining elements from two previous models, promised significant performance, reflecting Caudron’s characteristic innovation in racing aviation during that era.

The Coupe Deutch Challenge and its Fate

Despite being specially built for the Coupe Deutch competition, the C.561 was ultimately unable to participate. Persistent engine problems thwarted its aspirations, leading engineer Marcel Riffard to abandon further development of the project and shift his focus to more promising machines.

Technical Specifications

Modification C.561
Wingspan, m 6.67
Aircraft length, m 7.51
Aircraft height, m 1.80
Wing area, m2 6.89
Empty weight 600
Maximum takeoff weight 998
Engine type 1 Piston engine Renault 446
Power, hp 1 x 450
Maximum speed, km/h 500
Crew, crew members 1

Image and diagram gallery of the Caudron C.561

C.561
C.561
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C.561

How to cite this article:

APA: Caudron C.561 (). Caudron C.561. wp.archivoaereo.com. https://wp.archivoaereo.com/en/caudron-c-561-2/
VANCOUVER: Caudron C.561 [online]. wp.archivoaereo.com; [cited 2026-06-23]. Available at: https://wp.archivoaereo.com/en/caudron-c-561-2/
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Racing Aircraft Tags:French

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