14 CFR 23.2235: Structural strength.
Where this section sits in the code
- Title 14—Aeronautics and Space
- CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
- SUBCHAPTER C—AIRCRAFT
- PART 23—AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES
- Subpart C—Structures
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.
Collected 2026-08-27T02:24:20Z. Source file · JSON