PPRuNe Forums - View Single Post - AF66 CDG-LAX diverts - uncontained engine failure over Atlantic
Old 4th Oct 2017, 07:29
  #249 (permalink)  
procede
 
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I agree. Maximum thrust levels decrease with altitude.
During a step climb N1 will probably get close to 100% (max climb).
One more thing to mention is thermal stress, which could be higher at altitude. And then there are acoustic stresses...

Does the GP7000 have heating in the cone? Could well be that that failed...
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