| Manufacturer | IAF |
| Model | Tzukit |
| Modification | Tzukit |
| Country | Israel |
| Years | 1980 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 12.20 m |
| Length | 10.06 m |
| Height | 2.80 m |
| Wing area | 17.30 m2 |
| Zero fuel weight | - |
| Empty weight | 2550 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 3100 kg |
| Flight duration | - |
| Engine | 2 ТРД Turbomeca Marbore VI |
| Power | - |
| Thrust | 2 x 571 kN |
| Maximum speed | 683 km/h |
| Cruising speed | - |
| Rate of climb | - |
| Practical range | 1200 km |
| Service ceiling | 15000 m |
| Hovering ceiling | - |
| Crew | 1-2 |
