In late 1936, the company Société des Avions Caudron released a modernized version of the C.530 Rafale racing aircraft. The new aircraft, designated C.680, featured a fuselage shortened by 0.43 meters, new wings with reduced area, and retained the 152 hp (113 kW) four-cylinder air-cooled Renault Bengali Sport engine.
Initial Design and Specifications
Later that same year, the sole aircraft (registration number F-ANAM) was equipped with a more powerful 170 hp six-cylinder Renault 6Pfi engine. This upgrade led to a change in designation, becoming the C.684.
Evolution and Performance Enhancements
Even before the end of the year, another re-engining was performed. This time, a 220 hp Renault 6Q engine was installed, culminating in its final designation as the C.685 Super Rafale.
Technical Specifications
| Modification | C. 684 |
| Wingspan, m | 7.70 |
| Length, m | 7.07 |
| Height, m | 2.53 |
| Wing area, m2 | 9.00 |
| Empty weight | 640 |
| Maximum takeoff weight | 1000 |
| Engine type | 1 Piston engine Renault 6 Pfi |
| Power, hp | 1 x 170 |
| Maximum speed, km/h | 307 |
| Cruising speed, km/h | 270 |
| Practical range, km | 1550 |
| Service ceiling, m | 6800 |
| Crew | 2 |
Image and diagram gallery of the Caudron C.680 Rafale
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VANCOUVER: Caudron C.680 Rafale [online]. wp.archivoaereo.com; [cited 2026-06-09]. Available at: https://wp.archivoaereo.com/en/caudron-c-680-rafale-2/





