| Manufacturer | CAMS |
| Model | CAMS 52 |
| Modification | CAMS 52 |
| Country | France |
| Years | 1930 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 30.36 m |
| Length | 16.00 m |
| Height | 4.90 m |
| Wing area | 120.00 m2 |
| Zero fuel weight | - |
| Empty weight | 4400 kg |
| Maximum takeoff weight | 7618 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 Gnome & Rhone 9Akx |
| Power | 2 x 480 HP |
| Thrust | - |
| Maximum speed | 200 km/h |
| Cruising speed | 170 km/h |
| Rate of climb | - |
| Practical range | 1400 km |
| Service ceiling | 5000 m |
| Hovering ceiling | - |
| Crew | 5 |
