D-36, Series 1, 2A, 3A
The D-36, Series 1 turbofan engines are installed in the Yak-42 passenger airplanes. The D-36, Series 2A, 3A, turbofan engines are installed in the Аn-72 and Аn-74 transport airplanes. Perfect design and highly developed mass production ensure the engine’s quality and reliability. Easy maintenance and possibility of comprehensive operational diagnostics of the engine on wing bring about reliable engine on-condition operation.
Main advantages:
- Low specific fuel consumption;
- High reliability;
- Long service life;
- Low levels of noise and emissions of air pollutants;
- High maintainability and repairability ensured by the modular design;
- Universal mount for installing the engine on various airplanes in underwing or overwing,fuselage or side positions without changing the engine design.
Basic specifications:
| D-36, Series 1 and 2a | D-36, Series 3A | |
Emergency power condition (SLS, ISA+15°C): | ||
| Thrust, kgf (N) | 6500 (63765) | |
Takeoff power condition (SLS, ISA): | ||
| Thrust, kgf (N) | 6500 (63765) | 6500 (63765) |
| Specific fuel consumption, kg/kgf·h (kg/N·h) | 0.350 (0.0357) | 0.350 (0.0357) |
Cruise power condition (Н = 8000 m, Mfl = 0.75, ISA): | ||
| Thrust , kgf (N) | 1600 (15696) | 1600 (15696) |
| Specific fuel consumption, kg/kgf·h (kg/N·h) | 0.630 (0.0642) | 0,630 (0,0642) |
| Dry weight, kg | 1124 | 1124 |
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