| Type | Aircraft | |
| Company | SC A.S. Yakovlev Design Bureau | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.0
88.7
|
|
| Height (m) |
0.6
2.9
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
17.0
925
|
|
| Wingspan (Beam) (m) |
0.1
10.3
95
|
|
| Weights | ||
| Empty weight (kg) |
8
950
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
1,520
575,000
|
|
| Loaded weight (kg) |
5
1,300
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
230
28,165
|
|
| Сruise Speed (km/h) |
52
193
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
225
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
256
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
4,000
161,544
|
|
| Range (Ferry range) (km) |
4
1,000
40,700
|
|
| Propellers | ||
| Propellers (qt) |
1
1
8
|
|
| Prop blade number (qt) |
1
3
8
|
|
| Stat | ||
| Introduction | 1992 | |
| First flight | 20.10.1992 | |
