|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||3000|
|Delivery weight, kg||4400|
|Fan diameter, mm||1900|
Compared to the baseline engine, the PS-90A2 has a number of advantages including:
- durability and reliability increase by 1.5-2 times;
- significant life cycle cost reduction;
- reduction of maintenance manpower by 2 times.
Tu-204СМ medium-range aircraft.