{"data":{"id":"us/14-cfr-25.333","jurisdiction":"us","citation":"14 CFR 25.333","heading":"Flight maneuvering envelope.","body":"(a) General. The strength requirements must be met at each combination of airspeed and load factor on and within the boundaries of the representative maneuvering envelope (V-n diagram) of paragraph (b) of this section. This envelope must also be used in determining the airplane structural operating limitations as specified in § 25.1501.\n(b) Maneuvering envelope.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 25—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES","Subpart C—Structure"],"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":"ef2e104970571b27cdd7c39d9e9560bf422d17c02776770ceb939a02210a2d4e","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-25.331","next":"us/14-cfr-25.335"},"notice":"GroundRules: Original legal text. Not legal advice."}