| Manufacturer | LIPNUR |
| Model | NU-25 Kunang |
| Modification | NU-35 |
| Country | Indonesia |
| Years | 1958 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.60 m |
| Length | 7.20 m |
| Height | 1.77 m |
| Wing area | 9.53 m2 |
| Zero fuel weight | - |
| Empty weight | 229 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 337 kg |
| Flight duration | - |
| Engine | 1 VW |
| Power | 1 x 35 HP |
| Thrust | - |
| Maximum speed | 145 km/h |
| Cruising speed | 137 km/h |
| Rate of climb | 91 m/min |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 1 |
