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Old 28th Jun 2020, 06:33
  #14 (permalink)  
eckhard
 
Join Date: May 2005
Location: France
Age: 69
Posts: 1,143
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[QUOTE]With the large nose down pitching moments from the flaps the tail balancing loads are increased. Can be a critical design case for the tail structure.[/QUOTE]

If you’ve ever flown an Aztec or a Cessna 152, you’ll be surprised that they both pitch up quite strongly when the flaps are initially extended.
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