Мi-26Т
Performance | |
|---|---|
|
Max. speed
|
295 km/h |
|
Cruise speed
|
255 km/h |
|
Max. flight range with main fuel tanks
|
800 km |
|
Operational ceiling
|
4,600 m
|
|
Hover ceiling (OGE)
| 1,520 m |
Weight Parameters | |
|
Max. take-off weight
| 56,000 kg |
|
With underslung load
| 56,000 kg |
Max. Payload, kg | |
|
in transport cabin
|
20,000 kg
|
|
on external sling
|
20,000 kg |
Engine 2 х D-136 (2 х 11 400 h. p.) | |
|
Take-off power
|
h. p.
|
|
Contingency power
|
h. p. |
Cabin Dimensions |
|
Length
|
12.1 m
|
|
Width
|
3.29 m
|
|
Height
|
3.17 m
|
|
Volume
|
m3
|
Capacity: |
|
Aircrew
|
5–6
|
|
Passengers
|
82 |
