| Manufacturer | Cessna |
| Model | O-2 Skymaster |
| Modification | O-2A |
| Country | USA |
| Years | 1967 |
| Type | Reconnaissance aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.58 m |
| Length | 9.07 m |
| Height | 2.84 m |
| Wing area | 18.81 m2 |
| Zero fuel weight | - |
| Empty weight | 1292 kg |
| Maximum takeoff weight | 2449 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 Teledyne Continental 10-360C/D |
| Power | 2 x 210 HP |
| Thrust | - |
| Maximum speed | 320 km/h |
| Cruising speed | 232 km/h |
| Rate of climb | - |
| Practical range | 1706 km |
| Service ceiling | 5885 m |
| Hovering ceiling | - |
| Crew | 2 + 4 passengersа |
