{"data":{"id":"us/14-cfr-23.2235","jurisdiction":"us","citation":"14 CFR 23.2235","heading":"Structural strength.","body":"The structure must support:\n(a) Limit loads without—\n(1) Interference with the safe operation of the airplane; and\n(2) Detrimental permanent deformation.\n(b) Ultimate loads.","path":["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"],"source_url":"https://www.ecfr.gov/api/versioner/v1/full/2026-08-25/title-14.xml","current_through":"2026-08-25","vintage":"","retrieved_at":"2026-08-27T02:24:20Z","sha256":"c96a9fa0137ef22ed5b5f9379f919fcb110a296aed60f16b5de282a5372c0f27","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-23.2230","next":"us/14-cfr-23.2240"},"notice":"GroundRules: Original legal text. Not legal advice."}