D-36, Series 1, 2A, 3A
The D-36, Series 1, engines are used for passenger aircraft and the D-36, Series 2А and 3А engines are used for transport and convertible aircraft. The takeoff thrust is 6,500 kgf.
Quality and reliability of the engine are ensured by perfect design and high degree of maturity of mass production process.
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Main advantages of the engine:
- 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.
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Basic specifications:
| Emergency power condition (SLS, ISA +15 °C): |
| Thrust, kgf (kN) |
6,500 (63.76) |
| Takeoff power condition (SLS, ISA): |
| Thrust, kgf (kN) |
6,500 (63.76) |
| SFC, kg/kgf•h (kg/kN•h) |
0.350 (35.7) |
| Cruise power condition (H = 8,000 m, M= 0.75, ISA): |
| Thrust, kgf (kN) |
1,600 (15.69) |
| SFC, kg/kgf•h (kg/kN•h) |
0.630 (64.2) |
| Dry weight, kg |
1,124 |
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