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§23.351 Yawing conditions.

14 CFR 23 · Structure · Flight Loads · at 23-63 (current)

Text in force at 23-63: from 23-42, effective 4 Feb 1991.

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

56 FR 352 · Source

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