{"data":{"id":"us/14-cfr-29.735","jurisdiction":"us","citation":"14 CFR 29.735","heading":"Brakes.","body":"For rotorcraft with wheel-type landing gear, a braking device must be installed that is—\n(a) Controllable by the pilot;\n(b) Usable during power-off landings; and\n(c) Adequate to—\n(1) Counteract any normal unbalanced torque when starting or stopping the rotor; and\n(2) Hold the rotorcraft parked on a 10-degree slope on a dry, smooth pavement.","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 D—Design and Construction"],"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":"ba26c7bf9cabc666e3bcb938cc15fd869b772c3e5eda15b6047287ee61774921","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-29.733","next":"us/14-cfr-29.737"},"notice":"GroundRules: Original legal text. Not legal advice."}