PPRuNe Forums - View Single Post - Speed reduction from Vref+20 to Vref+15 in Boeing
Old 11th September 2018 | 12:30
  #6 (permalink)  
Goldenrivett
 
Joined: Jan 2014
Posts: 720
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From: N5109.2W10.5
It's unlikely be a landing distance limit - why have a maximum Vref increment on a very long runway with a strong headwind?
It's more likely to be a body attitude limit at touch down which has an unacceptable risk of a nose wheel impact before main body gear.
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