{"data":{"id":"us/14-cfr-27.493","jurisdiction":"us","citation":"14 CFR 27.493","heading":"Braked roll conditions.","body":"Under braked roll conditions with the shock absorbers in their static positions—\n(a) The limit vertical load must be based on a load factor of at least—\n(1) 1.33, for the attitude specified in § 27.479(a)(1); and\n(2) 1.0 for the attitude specified in § 27.479(a)(2); and\n(b) The structure must be designed to withstand at the ground contact point of each wheel with brakes, a drag load at least the lesser of—\n(1) The vertical load multiplied by a coefficient of friction of 0.8; and\n(2) The maximum value based on limiting brake torque.","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":"62ff579c6a61d684b0e410a8411ac7af4a3125854b56b5b62228c09033501e3f","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.485","next":"us/14-cfr-27.497"},"notice":"GroundRules: Original legal text. Not legal advice."}