| Manufacturer | Ikarus |
| Model | Kurir |
| Modification | Kurir |
| Country | Yugoslavia |
| Years | 1955 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 14.40 m |
| Length | 9.36 m |
| Height | 3.10 m |
| Wing area | 23.40 m2 |
| Zero fuel weight | - |
| Empty weight | 980 kg |
| Maximum takeoff weight | 1464 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Lycoming O-435-1 |
| Power | 1 x 180 HP |
| Thrust | - |
| Maximum speed | 180 km/h |
| Cruising speed | 147 km/h |
| Rate of climb | - |
| Practical range | 697 km |
| Service ceiling | 3960 m |
| Hovering ceiling | - |
| Crew | 2+2 |
