{"data":{"id":"us/14-cfr-27.671","jurisdiction":"us","citation":"14 CFR 27.671","heading":"General.","body":"(a) Each control and control system must operate with the ease, smoothness, and positiveness appropriate to its function.\n(b) Each element of each flight control system must be designed, or distinctively and permanently marked, to minimize the probability of any incorrect assembly that could result in the malfunction of the system.","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 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":"29ca1b1bf851d77ab017cf030b1bfe4e5dd763cc8fd2071c2c80967909d071f5","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.663","next":"us/14-cfr-27.672"},"notice":"GroundRules: Original legal text. Not legal advice."}