| Manufacturer | LFG Roland |
| Model | LFG Roland C.VIII |
| Modification | C.VIII |
| Country | Germany |
| Years | 1917 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.32 m |
| Length | 7.72 m |
| Height | 2.92 m |
| Wing area | 26.40 m2 |
| Zero fuel weight | - |
| Empty weight | 786 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1344 kg |
| Flight duration | 4 h |
| Engine | 1 Mercedes DIVa |
| Power | 1 x 260 HP |
| Thrust | - |
| Maximum speed | 180 km/h |
| Cruising speed | 160 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 5200 m |
| Hovering ceiling | - |
| Crew | 2 |
