| Manufacturer | CPA |
| Model | CPA-1 |
| Modification | CPA-1 |
| Country | France |
| Years | 1926 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 22.80 m |
| Length | 14.50 m |
| Height | 4.32 m |
| Wing area | 84.00 m2 |
| Zero fuel weight | - |
| Empty weight | 3350 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 4600 kg |
| Flight duration | - |
| Engine | 2 Hispano-Suiza 12 Ha |
| Power | 1 x 450 HP |
| Thrust | - |
| Maximum speed | 195 km/h |
| Cruising speed | 158 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 7000 m |
| Hovering ceiling | - |
| Crew | - |
