| Manufacturer | Grumman |
| Model | AA-5 |
| Modification | AA-5B |
| Country | USA |
| Years | 1971 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.60 m |
| Length | 6.70 m |
| Height | 2.40 m |
| Wing area | 13.00 m2 |
| Zero fuel weight | - |
| Empty weight | 680 kg |
| Maximum takeoff weight | 1090 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming O-360-A4K |
| Power | 1 x 180 HP |
| Thrust | - |
| Maximum speed | 265 km/h |
| Cruising speed | 230 km/h |
| Rate of climb | 259 m/min |
| Practical range | 1270 km |
| Service ceiling | 4200 m |
| Hovering ceiling | - |
| Crew | 2 |
