Federal Aviation Regulations
Sec. 23.391 — Control surface loads.
The control surface loads specified in §§23.397 through 23.459 are assumed to occur in the conditions described in §§23.331 through 23.351.[Doc. No. 4080, 29 FR 17955, Dec. 18, 1964, as amended by Amdt. 23–48, 61 FR 5145, Feb. 9, 1996]
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