| Manufacturer | IMAM |
| Model | Ro.41 |
| Modification | Ro.41 |
| Country | Italy |
| Years | 1934 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.81 m |
| Length | 6.90 m |
| Height | 2.68 m |
| Wing area | 19.50 m2 |
| Zero fuel weight | - |
| Empty weight | 1010 kg |
| Maximum takeoff weight | 1265 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Piaggio P.VII |
| Power | 1 x 390 HP |
| Thrust | - |
| Maximum speed | 320 km/h |
| Cruising speed | 254 km/h |
| Rate of climb | - |
| Practical range | 570 km |
| Service ceiling | 7750 m |
| Hovering ceiling | - |
| Crew | 1-2 |
