| Manufacturer | Jodel |
| Model | D.112 |
| Modification | D.112 |
| Country | France |
| Years | 1952 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 8.20 m |
| Length | 6.20 m |
| Height | - |
| Wing area | 12.75 m2 |
| Zero fuel weight | - |
| Empty weight | 325 kg |
| Maximum takeoff weight | 530 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Continental A-65 |
| Power | 1 x 65 HP |
| Thrust | - |
| Maximum speed | 180 km/h |
| Cruising speed | 160 km/h |
| Rate of climb | - |
| Practical range | 530 km |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 2 |
