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Old 3rd Oct 2011, 14:04
  #1089 (permalink)  
CONF iture
 
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It is important to know that if such a thrust increase was applied when the aircraft is already stalled, the longitudinal effect would bring the aircraft further into the stall, to a situation possibly unrecoverable.
AZR,
The way I see it is :
For obvious reasons a flight test cannot be risked.
AF447 was possibly unrecoverable the way the stall was initially engaged ...
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