| Manufacturer | Boulton Paul |
| Model | Boulton-Paul P.92 |
| Modification | P.92 |
| Country | United Kingdom |
| Years | 1939 |
| Type | Experimental aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 20.19 m |
| Length | 16.76 m |
| Height | 4.65 m |
| Wing area | 65.88 m2 |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | - |
| Normal takeoff weight | 8663 kg |
| Flight duration | - |
| Engine | 2 Rolls-Royce Vulture II |
| Power | 2 x 1710 HP |
| Thrust | - |
| Maximum speed | 597 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 11582 m |
| Hovering ceiling | - |
| Crew | - |
