| Manufacturer | Hughes |
| Model | XV-9 |
| Modification | XV-9A |
| Country | USA |
| Years | 1964 |
| Type | Experimental aircraft |
| Main rotor diameter | 16.76 m |
| Tail rotor diameter | - |
| Wingspan | - |
| Length | 13.72 m |
| Height | 3.66 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 3856 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 6940 kg |
| Flight duration | - |
| Engine | 2 General Electric YT64-GE-6 |
| Power | 2 x 2126 HP |
| Thrust | - |
| Maximum speed | 279 km/h |
| Cruising speed | 222 km/h |
| Rate of climb | - |
| Practical range | 240 km |
| Service ceiling | 3505 m |
| Hovering ceiling | - |
| Crew | 2 |
