| Manufacturer | IMAM |
| Model | Ro.58 |
| Modification | Ro.58 |
| Country | Italy |
| Years | 1942 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13.40 m |
| Length | 9.89 m |
| Height | 3.39 m |
| Wing area | 26.20 m2 |
| Zero fuel weight | - |
| Empty weight | 4350 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 6100 kg |
| Flight duration | - |
| Engine | 2 Daimler-Benz DB 601A-1 |
| Power | 2 x 1175 HP |
| Thrust | - |
| Maximum speed | 605 km/h |
| Cruising speed | 560 km/h |
| Rate of climb | - |
| Practical range | 1500 km |
| Service ceiling | 9800 m |
| Hovering ceiling | - |
| Crew | - |
