| Manufacturer | De Monge |
| Model | M-101 |
| Modification | M-101C2 |
| Country | France |
| Years | 1924 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.30 m |
| Length | 7.80 m |
| Height | 3.20 m |
| Wing area | 23.00 m2 |
| Zero fuel weight | - |
| Empty weight | 1015 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 1680 kg |
| Flight duration | - |
| Engine | 1 Gnome & Rhone 9Ac |
| Power | 1 x 420 HP |
| Thrust | - |
| Maximum speed | 235 km/h |
| Cruising speed | 195 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 7200 m |
| Hovering ceiling | - |
| Crew | - |
