| Manufacturer | Renard |
| Model | R-34 |
| Modification | R-34 |
| Country | Belgium |
| Years | 1933 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.20 m |
| Length | 6.90 m |
| Height | 2.45 m |
| Wing area | 22.00 m2 |
| Zero fuel weight | - |
| Empty weight | 740 kg |
| Maximum takeoff weight | 1147 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Armstrong Siddeley Lynx |
| Power | 1 x 260 HP |
| Thrust | - |
| Maximum speed | 215 km/h |
| Cruising speed | 176 km/h |
| Rate of climb | - |
| Practical range | 360 km |
| Service ceiling | 4600 m |
| Hovering ceiling | - |
| Crew | 2 |
