| Manufacturer | Heliopolis |
| Model | Gomhouria |
| Modification | Gomhouria Mk.8 |
| Country | Egypt |
| Years | 1952 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.60 m |
| Length | 7.85 m |
| Height | 2.05 m |
| Wing area | 13.50 m2 |
| Zero fuel weight | - |
| Empty weight | 520 kg |
| Maximum takeoff weight | 800 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Teledyne Continental O-300-A |
| Power | 1 x 145 HP |
| Thrust | - |
| Maximum speed | 225 km/h |
| Cruising speed | 205 km/h |
| Rate of climb | - |
| Practical range | 780 km |
| Service ceiling | 6000 m |
| Hovering ceiling | - |
| Crew | 2 |
