| Manufacturer | Mitsubishi |
| Model | Ki-46-I(II) |
| Modification | Ki-46-I |
| Country | Japan |
| Years | 1939 |
| Type | Reconnaissance plane |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 14.70 m |
| Length | 11.00 m |
| Height | 3.88 m |
| Wing area | 32.03 m2 |
| Zero fuel weight | - |
| Empty weight | 3379 kg |
| Maximum takeoff weight | - |
| Normal takeoff weight | 4822 kg |
| Flight duration | - |
| Engine | 2 Mitsubishi Ha-26-I |
| Power | - |
| Thrust | - |
| Maximum speed | 540 km/h |
| Cruising speed | 398 km/h |
| Rate of climb | 645 m/min |
| Practical range | 2100 km |
| Service ceiling | 10830 m |
| Hovering ceiling | - |
| Crew | - |
