

The world’s most efficient large aero engine Technical Data Configuration: Three-shaft turbofan High Pressure Compressor: 6 stages Noise: QC 0.5 departures/ QC 0.5 arrivals Overall Pressure Ratio: 50:1 High Pressure Turbine: Single stage Intermediate Pressure Turbine: Dual stage Intermediate Pressure Compressor: 8 stages Entry into service 2014 Low Pressure Turbine: 6 stages
Open the catalog to page 11 Page
1 Page
1 Page
1 Page
1 Page
4 Pages
2 Pages