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| Manufacturer | Hannover |
| Model | Hannover CL.II(IV) |
| Modification | CL.II |
| Country | Germany |
| Years | 1917 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.95 m |
| Length | 7.80 m |
| Height | 2.75 m |
| Wing area | 33.80 m2 |
| Zero fuel weight | - |
| Empty weight | 750 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1110 kg |
| Flight duration | 3.30 h |
| Engine | 1 Argus As III |
| Power | 1 x 180 HP |
| Thrust | - |
| Maximum speed | 165 km/h |
| Cruising speed | 141 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 7500 m |
| Hovering ceiling | - |
| Crew | 2 |
