{"data":{"id":"us/14-cfr-29.481","jurisdiction":"us","citation":"14 CFR 29.481","heading":"Tail-down landing conditions.","body":"(a) The rotorcraft is assumed to be in the maximum nose-up attitude allowing ground clearance by each part of the rotorcraft.\n(b) In this attitude, ground loads are assumed to act perpendicular to the ground.","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":"b76f531caa87911a2b02dfed1270e1c9394f1464585670c4414de2bc713f3122","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-29.479","next":"us/14-cfr-29.483"},"notice":"GroundRules: Original legal text. Not legal advice."}