| Manufacturer | Tachicawa |
| Model | Ki-17 |
| Modification | Ki-17 |
| Country | Japan |
| Years | 1935 |
| Type | Other |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 9.82 m |
| Length | 7.80 m |
| Height | 2.95 m |
| Wing area | 26.02 m2 |
| Zero fuel weight | - |
| Empty weight | 618 kg |
| Maximum takeoff weight | 900 kg |
| Normal takeoff weight | - |
| Flight duration | 3.45 h |
| Engine | 1 Hitachi Ha-12 ("Армейский тип 95" -7) |
| Power | 1 x 150 HP |
| Thrust | - |
| Maximum speed | 170 km/h |
| Cruising speed | 130 km/h |
| Rate of climb | - |
| Practical range | - |
| Service ceiling | 5300 m |
| Hovering ceiling | - |
| Crew | - |
