D-136-2
D-136-2 turboshaft engine is intended for improving the performance of civil transport helicopters.
D-136-2 engine has been developed on the basis of production engines D-136 series 1 and D-436T1 and features a high degree of commonalty with them, which will permit to radically reduce time and cost of building and certifying it. |
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Basic specifications:
| Emergency power rating (H=0, M=0, ISA+15°C): |
| Power rating, hp (kW) |
12500 (9190) |
| Maximum takeoff power rating (H=0, Mfl=0, ISA): |
| Power rating (at tAMB=30°C), hp (kW) |
11650 (8560) |
| Specific fuel consumption, kg/hp·h (kg/kW·h) |
0.198 (0.269) |
| Dry weight, kg |
1100 |
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