| Manufacturer | de Havilland |
| Model | DH.37 |
| Modification | DH-37 |
| Country | United Kingdom |
| Years | 1922 |
| Type | Light aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.28 m |
| Length | 8.53 m |
| Height | 2.86 m |
| Wing area | 36.97 m2 |
| Zero fuel weight | - |
| Empty weight | 961 kg |
| Maximum takeoff weight | 1505 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Rolls-Royce Falcon III |
| Power | 1 x 275 HP |
| Thrust | - |
| Maximum speed | 196 km/h |
| Cruising speed | 162 km/h |
| Rate of climb | - |
| Practical range | 450 km |
| Service ceiling | 6400 m |
| Hovering ceiling | - |
| Crew | 1 |
