| Manufacturer | North American |
| Model | A-27 |
| Modification | А-27 |
| Country | USA |
| Years | 1940 |
| Type | Attack plane |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.80 m |
| Length | 8.84 m |
| Height | 3.71 m |
| Wing area | 25.70 m2 |
| Zero fuel weight | - |
| Empty weight | 2050 kg |
| Maximum takeoff weight | 3040 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Wright R-1820-75 Cyclone |
| Power | 1 x 785 HP |
| Thrust | - |
| Maximum speed | 402 km/h |
| Cruising speed | 354 km/h |
| Rate of climb | - |
| Practical range | 1290 km |
| Service ceiling | 8500 m |
| Hovering ceiling | - |
| Crew | - |
