Take-off/ increased take-off thrust @ tamb < + 30 °C, Pamb > 730 mm Hg., H = 0), kgf | 16000 |
Cruise thrust (Н = 11 km, М = 0.8), kgf | 3500 |
SFC, kg/kgf • h | 0,595 |
Flight altitude, m | to 13100 |
Air temperature at ground level for starting and operation, °C | -47...+45 |
Aerodrome altitude, m | to 3500 |
Dry weight, kg | 2950 |
Delivery weight, kg | 4300 |
Fan diameter, mm | 1900 |
Compared to the baseline engine, use of the PS-90A3 may reduce the airline costs by 30% through:
- reducing maintenance manpower (to 0.2 MH per 1 flight hour);
- increasing the interval and reducing the scope of maintenance.
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IL-96-300 long-range aircraft;
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Tu-204-100, Tu-204-300, Tu-204С, Tu-214 medium-range passenger and cargo aircraft and their modifications.
Contact details
Deputy General Designer – Chief Designer, Aero Engines
Alexander V. Busygin


