| Manufacturer | Junkers |
| Model | Ju.252 |
| Modification | Ju.252a-1 |
| Country | Germany |
| Years | 1941 |
| Type | Transport airplane |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 34.10 m |
| Length | 25.10 m |
| Height | 5.75 m |
| Wing area | 122.60 m2 |
| Zero fuel weight | - |
| Empty weight | 13100 kg |
| Maximum takeoff weight | 24000 kg |
| Normal takeoff weight | 22500 kg |
| Flight duration | - |
| Engine | 3 Юнкеpс Jumo-211F |
| Power | 3 x 1340 HP |
| Thrust | - |
| Maximum speed | 435 km/h |
| Cruising speed | 385 km/h |
| Rate of climb | - |
| Practical range | 6500 km |
| Service ceiling | 6300 m |
| Hovering ceiling | - |
| Crew | - |
