StacksVerified U.S. regulatory reference

14 CFR §23.2235

Verified against eCFR.gov as of June 20, 2026View official text on eCFR.gov ↗
The structure must support:
  1. (a)Limit loads without—
    1. (1)Interference with the safe operation of the airplane; and
    2. (2)Detrimental permanent deformation.
  2. (b)Ultimate loads.