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Old 14th Mar 2009, 20:47
  #2084 (permalink)  
MU3001A
 
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This implies that if the Airbus was fitted with a RA-operated automatic thrust retard mechanism at 27', the Congonhas A319 would not have retained power on No 2 after landing?
This implies that RETARD is a necessary function of any A/T system, which itself is deemed to be a necessity presumably because it is safer than simply allowing pilots to control thrust directly.
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