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PS-90А Aero Engine

Baseline engine of the family

The PS-90A - the 4th generation Russian engine was certified in 1992.

Operated based on the technical condition

No limitations on MTBO and total lifetime.

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

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
Engine length, mm	4964
Fan diameter, mm	1900

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

Rossiya Government Squadron, Aviastar-TU, Transaero, Red Wings, Cubana, Air Koryo

Deputy General Designer – Chief Designer, Aero Engines

Alexander V. Busygin

Phone: 8 (342) 281-55-68

Fax: 8 (342) 281-54-77