| Manufacturer | IMAM |
| Model | Ro.30 |
| Modification | Ro.30 |
| Country | Italy |
| Years | 1932 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 15.75 m |
| Length | 10.24 m |
| Height | 3.50 m |
| Wing area | 33.36 m2 |
| Zero fuel weight | - |
| Empty weight | 1580 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 2630 kg |
| Flight duration | - |
| Engine | 1 Piaggio P.VIII |
| Power | 1 x 500 HP |
| Thrust | - |
| Maximum speed | 235 km/h |
| Cruising speed | 210 km/h |
| Rate of climb | - |
| Practical range | 1600 km |
| Service ceiling | 7500 m |
| Hovering ceiling | - |
| Crew | 3 |
