The CPA-1 was a bomber-reconnaissance aircraft developed by the French company Chantiers de Provence Aviation (CAP). This firm was established in 1924 as a division of Chantiers et Ateliers de Provence, located in Marseille.
The CPA-1 represented the company’s inaugural project. Its prototype, equipped with two 450 hp Hispano-Suiza 12 Ha engines, undertook its maiden flight in February 1926.
Development and First Flight
Tragically, during its testing phase, the aircraft crashed, leading to the immediate suspension of all further development work. This incident had a profound impact on the company’s future.
Tragic End and Company’s Fate
Chantiers de Provence Aviation survived only a few more years after the CPA-1’s accident. Ultimately, the company ceased operations in 1932, having failed to create a single additional aircraft.
Technical Specifications
| Modification | CPA-1 |
| Wingspan, m | 22.80 |
| Length, m | 14.50 |
| Height, m | 4.32 |
| Wing area, m2 | 84.00 |
| Empty weight | 3350 kg |
| Normal takeoff weight | 4600 kg |
| Engine type | 2 Hispano-Suiza 12 Ha piston engines |
| Power, hp | 1 x 450 hp |
| Maximum speed, km/h | 195 |
| Cruising speed, km/h | 158 |
| Service ceiling, m | 7000 |
| Crew | 4 crew members |
| Armament | Bomb load – up to 700 kg |
Image gallery of the CPA-1
