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PS-90А3 Aero Engine

PS-90A engine modification.

Certified in 2010 in accordance with AP-33.

The PS-90A3-powered aircraft meet ICAO 2006 emission and noise standards (Stage 4).

To be operated based on the technical condition.

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:

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.

Deputy General Designer – Chief Designer, Aero Engines

Alexander V. Busygin

Phone: 8 (342) 281-55-68

Fax: 8 (342) 281-54-77