For the purpose of improving the Mi-26T2 transport helicopter flight performance under higher environmental temperature and highland conditions designed is being a turboshaft gas turbine engine, designated D-136-2, based on the advanced D-436 turbofan gas generator, with a new full authority automatic control system of FADEC type, which now is passing bench tests.
| Takeoff (SLS, ISA) | |
| N, hp. | 12,200 |
| C, kg/hp/h | 0.210 |
| Dimensions, mm | 3,715 x 1,382 x 1,124 |
| Weight, dry, kg | 1,150 |
Applicability
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Mi-26
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Mi-26Т
