| Manufacturer | Junkers |
| Model | Ju.188A(C,D) |
| Modification | Ju.188a-2 |
| Country | Germany |
| Years | 1943 |
| Type | Bomber |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 22.00 m |
| Length | 14.95 m |
| Height | 4.45 m |
| Wing area | 56.00 m2 |
| Zero fuel weight | - |
| Empty weight | 9900 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 14500 kg |
| Flight duration | - |
| Engine | 2 Юнкерс Jumo-213А-1 |
| Power | - |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 450 km/h |
| Rate of climb | - |
| Practical range | 2385 km |
| Service ceiling | 9300 m |
| Hovering ceiling | - |
| Crew | - |
