|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.
IL-96-300 long-range aircraft;
Tu-204-100, Tu-204-300, Tu-204С, Tu-214 medium-range passenger and cargo aircraft and their modifications.