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The Trent XWB Story: Chris Fox

"What motivates me is the desire to get things right", Chris Fox, Quality Assurance Engineer, shares his experiences working on the world's most efficient ae.

Pratt & Whitney PW4098 (Boeing B777-300) Pratt & Whitney PW4000 is a family of high-bypass turbofan aircraft engines with certified thrust ranging from 52,000 to 99,040 lbf (230 to 441 kN). Maximum thrust: 77,440-99,040 lbf (344-441 kN)

Pratt & Whitney PW4098 (Boeing B777-300) Pratt & Whitney PW4000 is a family of high-bypass turbofan aircraft engines with certified thrust ranging from 52,000 to 99,040 lbf (230 to 441 kN). Maximum thrust: 77,440-99,040 lbf (344-441 kN)

PowerJet SaM146 is a turbofan engine produced by the PowerJet joint venture (not to be confused with Power Jets) between Snecma (Safran) of France and NPO Saturn of Russia. Developing 68–80 kN (15,000–18,000 lbf) of thrust, the SaM146 is used on the Sukhoi Superjet 100.

PowerJet is a turbofan engine produced by the PowerJet joint venture (not to be confused with Power Jets) between Snecma (Safran) of France and NPO Saturn of Russia. Developing kN lbf) of thrust, the is used on the Sukhoi Superjet

Garrett TFE731 (Honeywell TFE731)  (Lockheed Jetstar, Cessna Citation III, Dassault Falcon 900, Hawker 800, and Learjet 31)  Maximum thrust: 3500 lbf (15.6 kN)  Overall pressure ratio: 13:1. Fuel consumption: 875 lb. per hour. Specific fuel consumption: 0.5 lb/lbf-hr.  Thrust-to-weight ratio: 4.7:1

Garrett TFE731 (Honeywell TFE731) (Lockheed Jetstar, Cessna Citation III, Dassault Falcon 900, Hawker 800, and Learjet 31) Maximum thrust: 3500 lbf (15.6 kN) Overall pressure ratio: 13:1. Fuel consumption: 875 lb. per hour. Specific fuel consumption: 0.5 lb/lbf-hr. Thrust-to-weight ratio: 4.7:1

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