| Type | Aircraft | |
| Company | Mitsubishi Aircraft Corporation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
10.5
88.7
|
|
| Height (m) |
0.6
2.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
31.5
925
|
|
| Wingspan (Beam) (m) |
0.1
15.9
95
|
|
| Wing loading (kg/m2) |
3.1
91
829
|
|
| Weights | ||
| Empty weight (kg) |
8
1,840.2
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
2,860
575,000
|
|
| Loaded weight (kg) |
5
2,857.6
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
pilot |
| Capacity passengers (per.) |
1
6
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
338.0
28,165
|
at 2230 m |
| Сruise Speed (km/h) |
52
309.0
3,087
|
at 75% power and 2230 m |
| Power | ||
| Power/mass (hp/kg) |
0.0
0.2
22.1
|
|
| Total Power (hp) |
0.4
690
60,000
|
2 powerplants 345 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,858
161,544
|
|
| Range (Ferry range) (km) |
4
1,046
40,700
|
at 62.5% power and 3050 m |
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
250
36,000
|
|
| Time to altitude (min) |
0.6
8
105
|
to 3050 m |
| Stat | ||
| Number built (qt) |
0
11
43,000
|
|
| Introduction | 1934 | |
| First flight | 26.06.1934 | |
| Stop production | 1951 | |
