{"data":{"id":"us/14-cfr-29.493","jurisdiction":"us","citation":"14 CFR 29.493","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 § 29.479(a)(1); and\n(2) 1.0, for the attitude specified in § 29.479(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 of 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 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":"6cfaa01d78449bf6d7da1881759d52a8f8ed399d1e21c2ce6b79c0e66a2c1680","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-29.485","next":"us/14-cfr-29.497"},"notice":"GroundRules: Original legal text. Not legal advice."}