{"data":{"id":"us/14-cfr-23.2230","jurisdiction":"us","citation":"14 CFR 23.2230","heading":"Limit and ultimate loads.","body":"The applicant must determine—\n(a) The limit loads, which are equal to the structural design loads unless otherwise specified elsewhere in this part; and\n(b) The ultimate loads, which are equal to the limit loads multiplied by a 1.5 factor of safety unless otherwise specified elsewhere in this part.","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":"048c3b0f8a0061f17180db3d55b091d426fe4afcd6fcec43f41ea73857e9974c","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-23.2225","next":"us/14-cfr-23.2235"},"notice":"GroundRules: Original legal text. Not legal advice."}