| Manufacturer | Junkers |
| Model | G.23 |
| Modification | G23 |
| Country | Germany |
| Years | 1924 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 28.50 m |
| Length | 15.23 m |
| Height | 5.40 m |
| Wing area | 89.00 m2 |
| Zero fuel weight | - |
| Empty weight | 3600 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 6000 kg |
| Flight duration | - |
| Engine | 1 BMW IIIa + Mercedes Benz D.I |
| Power | 1 x 185 + 2 x 100 HP |
| Thrust | - |
| Maximum speed | 175 km/h |
| Cruising speed | 150 km/h |
| Rate of climb | - |
| Practical range | 1000 km |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 2 |
