| Manufacturer | Fouga |
| Model | CM.170 Magister |
| Modification | CM.170-1 |
| Country | France |
| Years | 195 |
| Type | Attack aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.40 m |
| Length | 10.06 m |
| Height | 2.80 m |
| Wing area | 17.30 m2 |
| Zero fuel weight | - |
| Empty weight | 2150 kg |
| Maximum takeoff weight | 3200 kg |
| Normal takeoff weight | 2850 kg |
| Flight duration | - |
| Engine | 2 Turbomeca Marbore IIA |
| Power | - |
| Thrust | 3.92 kN |
| Maximum speed | - |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1200 km |
| Service ceiling | 11000 m |
| Hovering ceiling | - |
| Crew | 2 |
