Trent 7000
1Pages

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Catalog excerpts

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

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