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Old 25th Mar 2009, 06:58
  #250 (permalink)  
denkraai
 
Join Date: Jun 2005
Location: Netherlands
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LSAS

Below 100' RA the MD11 LSAS control law implements a pitch attitude limiting function.Also the PNL (positive nose lowering) function of LSAS pushes the nose down at wheel spinup.
My experience is that every landing on the MD11 varies greatly with flapsetting, CG value, and wind (especially X-wind), and overspeed makes it very difficult to land.
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