| Manufacturer | Grumman |
| Model | C-2 Greyhound |
| Modification | С-2А |
| Country | USA |
| Years | 1964 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 24.56 m |
| Length | 17.32 m |
| Height | 4.86 m |
| Wing area | 65.03 m2 |
| Zero fuel weight | - |
| Empty weight | 16486 kg |
| Maximum takeoff weight | 26082 kg |
| Normal takeoff weight | 22450 kg |
| Flight duration | - |
| Engine | 2 Allison Т56-А-425 |
| Power | 2 x 4912 HP |
| Thrust | - |
| Maximum speed | 574 km/h |
| Cruising speed | 465 km/h |
| Rate of climb | - |
| Practical range | 2891 km |
| Service ceiling | 9144 m |
| Hovering ceiling | - |
| Crew | 4 |
