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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Text in force at 23-63: from 23-42, effective 4 Feb 1991.
56 FR 352 · Source
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