| Type | Aircraft | |
| Company | SC A.S. Yakovlev Design Bureau | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8
88.7
|
|
| Height (m) |
0.6
2.5
50.1
|
tail up |
| Wings | ||
| Wing area (m2) |
1.1
23
925
|
|
| Wingspan (Beam) (m) |
0.1
12.8
95
|
|
| Weights | ||
| Empty weight (kg) |
8
670
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
912
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
3
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
192
28,165
|
|
| Сruise Speed (km/h) |
52
152
3,087
|
|
| Power | ||
| Total Power (hp) |
0.4
200
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
4,275
161,544
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
6.5
105
|
to 1000 m |
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| First flight | 1931 | |
