| Manufacturer | Dzialowskich |
| Model | DKD-I |
| Modification | DKD-I |
| Country | Poland |
| Years | 1926 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.40 m |
| Length | 5.50 m |
| Height | 1.90 m |
| Wing area | 11.50 m2 |
| Zero fuel weight | - |
| Empty weight | 220 kg |
| Maximum takeoff weight | 395 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Haacke |
| Power | 1 x 30 HP |
| Thrust | - |
| Maximum speed | 120 km/h |
| Cruising speed | 100 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 2 |
