Tachikawa Ki-36
Liaison Aircraft
The Tachikawa Ki-36 is a single-engine two-seat liaison aircraft produced by the Japanese manufacturer Tachikawa Aircraft Company. Primary operator of the Ki-36 was the Imperial Japanese Army Air Force.
| Propulsion | 1 Radial Engine |
| Engine Model | Hitachi Ha-13a |
| Engine Power | 375 kW | 503 hp |
| Speed | 348 km/h | 188 kts
216 mph |
| Service Ceiling | 8.150 m | 26.739 ft |
| Range | 1.235 km | 667 NM
768 mi. |
| Empty Weight | 1.247 kg | 2.749 lbs |
| max. Takeoff Weight | 1.660 kg | 3.660 lbs |
| Wing Span | 11,80 m | 38 ft 9 in |
| Wing Area | 20,0 m² | 215 ft² |
| Length | 8,00 m | 26 ft 3 in |
| Height | 3,64 m | 11 ft 11 in |
| First Flight | 20.04.1938 |
| Production Status | out of production |
| Total Production | 1389 |
| Data for (Version) | Tachikawa Ki-36 |
| Variants | Tachikawa Ki-55 |
