| Manufacturer | Manicatide |
| Model | RM-4 |
| Modification | RM-4 |
| Country | Romania |
| Years | 1932 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.00 m |
| Length | 8.30 m |
| Height | - |
| Wing area | 12.00 m2 |
| Zero fuel weight | - |
| Empty weight | 175 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 250 kg |
| Flight duration | - |
| Engine | 1 Indian |
| Power | 1 x 12 HP |
| Thrust | - |
| Maximum speed | 85 km/h |
| Cruising speed | 65 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
