| Manufacturer | Caudron |
| Model | Caudron C-D-E |
| Modification | Caudron C(D) |
| Country | France |
| Years | 1912 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.00 (9.70) m |
| Length | 6.70 (6.70) m |
| Height | - |
| Wing area | 24.50 (24.00) m2 |
| Zero fuel weight | - |
| Empty weight | (220) kg |
| Maximum takeoff weight | (350) kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Anzani (Gnome) |
| Power | 1 x 45 (50) HP |
| Thrust | - |
| Maximum speed | 90 (90) km/h |
| Cruising speed | 80 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 (1) |
