PPRuNe Forums - View Single Post - Maximum civil aircraft pitch angle during normal operation
Old 20th Feb 2007, 17:18
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Mad (Flt) Scientist
 
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Since the regulatory requirements for single engine climb capability aren't going to change (significantly) and no-one is going to design for excess performance just for the sake of it, chances are that the performance-limited pitch attitudes will be pretty similar.

But in any case the 20 degree number seems to be a pax comfort limit anyway.
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