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B757 Assumed temperature T/O thrust time limit?
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14th February 2012 | 09:55
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rudderrudderrat
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Hi Jonty,
Do you really believe that Chapter 1 Limitations, 1.7 Engine, 1.7.2 EGT limits is saying the material used for the turbine blades is happy for continuous use at 849 degs C?
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