| Manufacturer | IMAM |
| Model | Ro.63 |
| Modification | Ro.63 |
| Country | Italy |
| Years | 1940 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13.50 m |
| Length | 9.60 m |
| Height | 2.35 m |
| Wing area | - |
| Zero fuel weight | - |
| Empty weight | 620 kg |
| Maximum takeoff weight | 1060 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Hirth HM 508D |
| Power | 1 x 250 HP |
| Thrust | - |
| Maximum speed | 203 km/h |
| Cruising speed | 164 km/h |
| Rate of climb | - |
| Practical range | 900 km |
| Service ceiling | 6800 m |
| Hovering ceiling | - |
| Crew | 2 |
