PS-90A2 is one of the PS-90A modifications with significant upgrade of some components and systems providing improvement of its operating performance. The engine is on a level with modern world standards.

Modular design, high commonality, turbofan, bypass, two-shaft, mixed flow with a thrust reverser in a fan duct and silencing system.

It has been designed for passenger and cargo transportation by long-haul airplanes, such as IL-96-300 and mid-haul airplanes TU-204, TU-214, IL-76TD.

Fuel consumption does not exceed 7000...8000 kg per one flight hour for IL-96-300 aircraft and 3500 kg per one flight hour for Tu-204 aircraft.


Thrust, kg:
-take-off: TH< +30 îC , PH > 730 mm Hg, H=0
-cruise: H=11 km, MÌ=0.8

16 000
3 500
Specific fuel consumption (with real nozzle), kg / h.p. hour  0.595
Flight altitude, mup to 13 100
Air temperature at sea level (for start and operation), C -47...+45
Airfield height (versus sea level) , mup to 3 500
Length of the engine, mm4964
Fan tip diameter, mm 1900
  Dry weight, kg 3 000
   Weight as delivered, kg 4 230


Advantages of the PS-90A2 engine compared to the prototype

  • Cost reduction of life cycle up to 37 %;
  • Compliance with the new ICAO (Chapter 4) noise regulations;
  • Reliability increase by 1.5 ... 2;
  • Conformity to the ETOPS requirements for two-engine airplanes on continuous 120-min long-distance flight and above-ocean routes;
  • In-field operation maintenance cost is double reduced;
  • Certification according to the AP-33 aviation regulations (analogue of the American FAR-33 and European JAR-33);
  • Localization of destruction in case of fan blade out;
  • Thrust forcing possibility - to 18000 kgf;
  • In-field stability of parameters;
  • Increase of fire safety due to some fuel accessories replacement with pneumatic ones.

If you would like to receive further information concerning our engines, please fill in the questionnaire.

See also PS-90A2 in pictures.