Design and Characteristics of the Couzinet 30
The Couzinet 30 was a light transport aircraft, designed by René Couzinet in early 1930. This model was developed from the Couzinet 20, marking an evolution in his aeronautical creations. It was a small, four-seater wooden low-wing monoplane, featuring fixed landing gear.
The aircraft was powered by three Salmson 9Ad engines, each providing 40 horsepower. This triple-engine configuration aimed to offer a balance of power and reliability for its intended use.
Maiden Flight and Original Purpose
The inaugural flight of the Couzinet 30 took place on October 21, 1930. Initially, it was primarily envisioned for use in tourist flights, leveraging its lightweight design and four-person capacity. It was hoped to attract a growing market in recreational aviation.
Operational History and Unique Fate
Despite its characteristics, the Couzinet 30 failed to attract commercial customers. Due to the lack of orders, the sole example built, bearing the registration number F-ALIG, was personally utilized by the designer himself, René Couzinet, until 1935.
Technical Specifications
| Modification | Couzinet 30 |
| Wingspan, m | 16.16 |
| Aircraft length, m | 11.41 |
| Aircraft height, m | 2.70 |
| Wing area, m2 | 34.40 |
| Empty weight | 1074 |
| Maximum takeoff weight | 1815 |
| Engine type | 3 Piston engine Salmson 9Ad |
| Power, hp | 3 x 40 |
| Maximum speed, km/h | 178 |
| Cruising speed, km/h | 145 |
| Practical range, km | 2000 |
| Practical ceiling, m | 3600 |
| Crew | 4 |
Image and diagram gallery of the Couzinet 30
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