Aeroderivative Gas Turbine PS-90А3
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.
- Weight (kg)2950
- length (m)4.964
- Take-off thrust (kgf)16000
- Cruise thrust (kgf)3500
- Specific fuel consumption (kg/kgf.hr)0.595
- Max. Flight altitude (m)13100
- Fan diameter (m)1.9