| Manufacturer | SPAD |
| Model | S.41 |
| Modification | S.41 |
| Country | France |
| Years | 1922 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.68 m |
| Length | 6.65 m |
| Height | 2.76 m |
| Wing area | 26.40 m2 |
| Zero fuel weight | - |
| Empty weight | 887 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1307 kg |
| Flight duration | - |
| Engine | 1 Hispano-Suiza 8Fb |
| Power | 1 x 300 HP |
| Thrust | - |
| Maximum speed | 238 km/h |
| Cruising speed | 205 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 6850 m |
| Hovering ceiling | - |
| Crew | - |
