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| Manufacturer | Consolidated |
| Model | P-30 (PB-2) |
| Modification | P-30 |
| Country | USA |
| Years | 1933 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13.39 m |
| Length | 9.14 m |
| Height | 2.51 m |
| Wing area | 27.58 m2 |
| Zero fuel weight | - |
| Empty weight | 1953 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 2560 kg |
| Flight duration | - |
| Engine | 1 Curtiss V-1570-61 Conqueror |
| Power | 1 x 700 HP |
| Thrust | - |
| Maximum speed | 441 km/h |
| Cruising speed | 346 km/h |
| Rate of climb | - |
| Practical range | 818 km |
| Service ceiling | 8535 m |
| Hovering ceiling | - |
| Crew | - |
