PS-90A-76 Aircraft Engine

The PS-90A-76 aero engine (PS - Pavel Soloviev) is a modification of the PS-90A turbofan. It extends service life of the large fleet of the IL-76 transport airplanes and raises their efficiency by installation of the PS-90A-76 engine instead of the D-30KP. 

It is a high-bypass-ratio, two-shaft turbofan, with mixed flow and a thrust reverser in a fan duct and noise absorbing system. 


The aero engine is intended to power IL-76 cargo aircraft and its modifications.

The engine was certified in 2003.

In 2004 JSC "UEC-Perm Engines" launched the serial production of the engine.

PS-90A-76 engines are currently in service at  three (3) Airlines.


Thrust, kg:
-take-off: TH< +30°C , PH > 730 mm Hg, H=0
-cruise: Í=11 km, Ì=0.8

Specific fuel consumption (with real nozzle), kg/kgf hour0.595
Flight altitude, m Up to 13100
Air temperature at sea level (for start and operation), ° Ñ -47...+45
Airfield height (versus sea level), m Up to 3500
Engine length, mm 4964
Fan tip diameter, mm 1900
Dry weight, kg  2950
 Weight as delivered, kg 4 160

Advantages of the PS-90A-76 turbofan engine compared to D-30KP

  • Conformity of ecological parameters on emission and noise to ICAO  regulations
  • Increase of reliability and life
  • Improvement of efficiency
  • Availability of thrust augmentation up to 16000 kg

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

See also PS-90A-76 in pictures.