1. Regulations
  2. title 14
  3. chapter I
  4. part 23
  5. subpart C
  6. subjgrp 22
  7. § 23.2235

View all text of Subjgrp 22 [§ 23.2235 - § 23.2245]

§ 23.2235 - Structural strength.

The structure must support:

(a) Limit loads without—

(1) Interference with the safe operation of the airplane; and

(2) Detrimental permanent deformation.

(b) Ultimate loads.

AUTHORITY: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704, Pub. L. 113-53, 127 Stat. 584 (49 U.S.C. 44704) note.

SOURCE: Doc. No. FAA-2015-1621, Amdt. 23-64, 81 FR 96689, Dec. 30, 2016, unless otherwise noted.

CITE AS: 14 CFR 23.2235