| Manufacturer | Junkers |
| Model | Ju.88a-1(2) |
| Modification | Ju.88a-1 |
| Country | Germany |
| Years | 1936 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 18.40 m |
| Length | 14.35 m |
| Height | 5.30 m |
| Wing area | 52.50 m2 |
| Zero fuel weight | - |
| Empty weight | 7700 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 10400 kg |
| Flight duration | - |
| Engine | 2 Юнкерс Jumo-211B-1 or G-1 |
| Power | 2 x 1200 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 350 km/h |
| Rate of climb | - |
| Practical range | 1690 km |
| Service ceiling | 9800 m |
| Hovering ceiling | - |
| Crew | - |
