| Manufacturer | Rockwell |
| Model | IAI-1121 Jet Commander |
| Modification | IAI-1121 |
| Country | USA, Israel |
| Years | 1963 |
| Type | Passenger aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 13.65 m |
| Length | 15.36 m |
| Height | 4.81 m |
| Wing area | 28.64 m2 |
| Zero fuel weight | - |
| Empty weight | 5210 kg |
| Maximum takeoff weight | 9276 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 2 General Electric CJ610-1 |
| Power | - |
| Thrust | 2 x 1293 kN |
| Maximum speed | 895 km/h |
| Cruising speed | 850 km/h |
| Rate of climb | - |
| Practical range | 3200 km |
| Service ceiling | 12400 m |
| Hovering ceiling | - |
| Crew | 2 |
