{"data":{"id":"us/14-cfr-27.341","jurisdiction":"us","citation":"14 CFR 27.341","heading":"Gust loads.","body":"The rotorcraft must be designed to withstand, at each critical airspeed including hovering, the loads resulting from a vertical gust of 30 feet per second.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 27—AIRWORTHINESS STANDARDS: NORMAL 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":"9a7db903722dbcc6f13938fa64d5f1c20da66d906fe98ee69329939668ba999f","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.339","next":"us/14-cfr-27.351"},"notice":"GroundRules: Original legal text. Not legal advice."}