D-136/D-136 series 1
The D-136 and D-136 series 1, turboshaft engines are used to power the civil transport helicopters. Perfect design and highly developed production ensure the engine`s quality and reliability.
Easy maintenance and high repairability are ensured by a modular design of the engine. |
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Main advantages of the engine:
- Low specific fuel consumption;
- High reliability;
- High power;
- Easy maintenance and high repairability;
- Low weight-to-power ratio.
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Basic specifications:
| Maximum takeoff power conditions (SLS, ISA) |
| Power, shp (kW) |
11400 (8382) |
| Specific fuel consumption, kg/hp•h (kg/kW•h) |
0.194 (0.263) |
| Cruise power conditions (H=4600 m, Mfl=0,13; ISA) |
| Power, shp (kW) |
6100 (4486) |
| Specific fuel consumption, kg/hp•h (kg/kW•h) |
0.230 (0.312) |
| Dry weight, kg |
1077 |
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