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FAA Federal Aviation Regulations (FARS, 14 CFR)

FARs   >   Part 23   >   Section 351 - Yawing conditions

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The airplane must be designed for yawing loads on the vertical surfaces resulting from the loads specified in §§23.441 through 23.445.

[Doc. No. 4080, 29 FR 17955, Dec. 18, 1964; 30 FR 258, Jan. 9, 1965, as amended by Amdt. 23-42, 56 FR 352, Jan. 3, 1991]

 

 

 

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