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§23.643 Rib tests.

14 CFR 23 · Design and Construction · Wings · at 23-63 (current)

Text in force at 23-63: from 23-0, effective 1 Feb 1965.

(a) Rib tests must simulate the conditions in the airplane with respect to-- (1) Torsional rigidity of spars; (2) Fixity conditions; (3) Lateral supports; and (4) Attachment to spars. (b) The effects of ailerons and high lift devices must be accounted for.

29 FR 17955 · Source

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