| Manufacturer | Tachikawa |
| Model | Ki-106 |
| Modification | Ki-106 |
| Country | Japan |
| Years | 1945 |
| Type | Fighter |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 11.238 m |
| Length | 9.95 m |
| Height | 3.56 m |
| Wing area | 21.02 m2 |
| Zero fuel weight | - |
| Empty weight | 2948 kg |
| Maximum takeoff weight | 4450 kg |
| Normal takeoff weight | 3900 kg |
| Flight duration | - |
| Engine | 1 Nakajima Ha-45-21 |
| Power | 1 x 1990 HP |
| Thrust | - |
| Maximum speed | 620 km/h |
| Cruising speed | 500 km/h |
| Rate of climb | - |
| Practical range | 1100 km |
| Service ceiling | 10000 m |
| Hovering ceiling | - |
| Crew | - |
