{"data":{"id":"us/14-cfr-29.341","jurisdiction":"us","citation":"14 CFR 29.341","heading":"Gust loads.","body":"Each rotorcraft must be designed to withstand, at each critical airspeed including hovering, the loads resulting from vertical and horizontal gusts of 30 feet per second.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT","Subpart C—Strength Requirements"],"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":"9915bd72d5a95a54c07db17c54676798cab319629dc757cd587abd55c56f448d","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-29.339","next":"us/14-cfr-29.351"},"notice":"GroundRules: Original legal text. Not legal advice."}