§23.2235. Structural strength.

14 C.F.R. § 23.2235

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.

Notes, amendments, and revision history

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.