| Manufacturer | Grumman |
| Model | AA-1 |
| Modification | AA-1C |
| Country | USA |
| Years | 1963 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 7.46 m |
| Length | 5.86 m |
| Height | 2.29 m |
| Wing area | 9.38 m2 |
| Zero fuel weight | - |
| Empty weight | 455 kg |
| Maximum takeoff weight | 726 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming O-235-L2C |
| Power | 1 x 115 HP |
| Thrust | - |
| Maximum speed | 234 km/h |
| Cruising speed | 208 km/h |
| Rate of climb | 213 m/min |
| Practical range | 711 km |
| Service ceiling | 3505 m |
| Hovering ceiling | - |
| Crew | 2 |
