|
| UT-2 |  |
|
| Training aircraft | ||
 |
  |
 |
|
|
Specification: | |
|
Year deployed
Wing span, m Lenght, m Height, m Wings area, m2 Weight, kg - empty aircraft - normal take-off - maximum take-off Engine Power, hp Maximum speed, km/h Cruising speed, km/h Range, km Rate of climb, m/min Service ceiling, m Crew |
-
1936 - 10.20 - 7.00 - 2.55 - 17.20 - 616 - 856 - 938 - 1 PE M-11E - 1 У 150 - 230 - 205 - 500 - - 3500 - 2 |
|
