
| At take-off power (sea level, static, ISA): | |
| Thrust, kg(f) | 6500 |
| Specific fuel consumption, kg/ kg(f)-h | 0.350 |
| Air flow rate, kg/s | 260 |
| By-pass ratio | 5.6 |
| Overall compressor pressure ratio | 20.0 |
| TIT, K | 1450 |
| At maximum cruise power (H=8000m, Mfl=0.75, ISA): | |
| Thrust, kg(f) | 1600 |
| Specific fuel consumption, kg/kg(f)-h | 0.620 |
| Overall dimensions, mm: | 3469x1541x1711 |
| Dry mass, kg | 110 |
The engine is listed by Motor Sich as a past rather than current programme, although small numbers of Mi-26 helicopters continue to be exported, the most recent (2006-7) being three Mi-26T multirole transports for Venezuela.The D-136 is composed of 10 modules, each of which (except for the main module) can be removed and replaced without disturbing neighbouring modules on an installed engine. Five of the gas-generator modules are identical with those of the D-36.















