| Manufacturer | Dayton-Wright |
| Model | TA-5 |
| Modification | TA-5 |
| Country | USA |
| Years | 1923 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 10.60 m |
| Length | - |
| Height | - |
| Wing area | 26.50 m2 |
| Zero fuel weight | - |
| Empty weight | - |
| Maximum takeoff weight | 1845 kg |
| Normal takeoff weight | 1014 kg |
| Flight duration | - |
| Engine | 1 Lawrance J-1 |
| Power | 1 x 220 HP |
| Thrust | - |
| Maximum speed | 167 km/h |
| Cruising speed | 150 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | - |
| Hovering ceiling | - |
| Crew | 2 |
