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Old 28th August 2010 | 16:53
  #20 (permalink)  
zulu_01
 
Joined: Apr 2008
Posts: 40
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From: FL 600
CAS/Mach limits
the CAS limits are for the sea level performance primarily due to flutter/drag/temp/structural limits.
the M.no limits are applicable at higher altitude and again due to Flutter/temp/engine intake design etc.
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