| Manufacturer | Central Aircraft |
| Model | Centaur IV |
| Modification | Centaur IVA |
| Country | United Kingdom |
| Years | 1919 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.43 m |
| Length | 7.54 m |
| Height | - |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 408 kg |
| Maximum takeoff weight | 635 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Anzani |
| Power | 1 x 100 HP |
| Thrust | - |
| Maximum speed | 121 km/h |
| Cruising speed | 105 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 3 |
