D-36, Series 1, 2a, 3a Turbofan Engines

The D-36, series 1, turbofan engines are installed in Yak-42 passenger airplanes. The D-36, series 2A, 3A, turbofan engines are installed in An-72 and An-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 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

BASIC SPECIFICATIONS
 D-36 Ser. 1, Ser.          2A D-36, Ser. 3A
Emergency power condition (SLS, ISA +15 °C): 
Thrust, kgf (kN)                   6500 (63.76)
Takeoff power condition (SLS, ISA): 
Thrust, kgf (kN)          6500 (63.76) 6500 (63.76)
Specific fuel consumption, 
kg/kgf•h (kg/kN•h)
  0.350 (35.7)                 0.350 (35.7)
Cruise power condition (H = 8000 m, Mfl = 0.75, ISA):
Thrust, kgf (kN)   1600 (15.69)               1600 (15.69)
Specific fuel consumption, 
kg/kgf•h (kg/kN•h)
   0.630 (64.2)                0.630 (64.2)
Dry weight, kg       1124                            1124
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