| Manufacturer | Junkers |
| Model | Ju.88a-4(17) |
| Modification | Ju.88a-4 |
| Country | Germany |
| Years | 1940 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 20.00 m |
| Length | 14.40 m |
| Height | 4.85 m |
| Wing area | 54.50 m2 |
| Zero fuel weight | - |
| Empty weight | 9870 kg |
| Maximum takeoff weight | 14000 kg |
| Normal takeoff weight | 12115 kg |
| Flight duration | - |
| Engine | 2 Юнкерс Jumo-211J-1 or J-2 |
| Power | 2 x 1340 HP |
| Thrust | - |
| Maximum speed | 467 km/h |
| Cruising speed | 400 km/h |
| Rate of climb | - |
| Practical range | 2710 km |
| Service ceiling | 8200 m |
| Hovering ceiling | - |
| Crew | - |
