| Manufacturer | Caudron |
| Model | Caudron G.IV |
| Modification | G.IV В.2 |
| Country | France |
| Years | 1915 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 17.20 m |
| Length | 7.20 m |
| Height | 2.60 m |
| Wing area | 36.80 m2 |
| Zero fuel weight | - |
| Empty weight | 500 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1330 kg |
| Flight duration | 3.30 h |
| Engine | 1 Le Rhone 9C |
| Power | 1 x 80 HP |
| Thrust | - |
| Maximum speed | 132 km/h |
| Cruising speed | 114 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 4300 m |
| Hovering ceiling | - |
| Crew | - |
