| Manufacturer | Culver |
| Model | PQ-14 |
| Modification | PQ-14B |
| Country | USA |
| Years | 1943 |
| Type | Unmanned aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.14 m |
| Length | 5.94 m |
| Height | 2.54 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | - |
| Normal takeoff weight | 830 kg |
| Flight duration | - |
| Engine | 1 Franklin O-300-11 |
| Power | 1 x 150 HP |
| Thrust | - |
| Maximum speed | 300 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 580 km |
| Service ceiling | 5200 m |
| Hovering ceiling | - |
| Crew | - |
