{"data":{"id":"us/14-cfr-23.2215","jurisdiction":"us","citation":"14 CFR 23.2215","heading":"Flight load conditions.","body":"The applicant must determine the structural design loads resulting from the following flight conditions:\n(a) Atmospheric gusts where the magnitude and gradient of these gusts are based on measured gust statistics.\n(b) Symmetric and asymmetric maneuvers.\n(c) Asymmetric thrust resulting from the failure of a powerplant unit.","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":"875bfd72c611f348e09026004267da7e0459328a67757a0c55f8cfaf3683ab9e","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-23.2210","next":"us/14-cfr-23.2220"},"notice":"GroundRules: Original legal text. Not legal advice."}