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.
| Engine | AI-136Т | D-136Т-2/АІ-136Т-2 |
| 2.5 minutes power with one engine running out of power | ||
| Power, hp. | – | 40 |
| Maximum 30-minute power H=0, Vn=0, ICA | ||
| Power, hp. | 11 400 | |
| Up to temperature supported, 0С. | 30 | 40 |
| Takeoff power H=0, Vn=0, ICA | ||
| Power, hp. | 10 000 | |
| Up to temperature supported, 0С. | 22 | 40 |
| Specific fuel consumption, kg/hp/h | 0,210 | |
| Weight, dry, kg | 1150 | |
| Dimensions, mm | 3703 x 1124 x 1146 | |
| Assigned resource, h | 6 000 | 12 000 |
Applicability
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Mi-26
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Mi-26Т