{"data":{"id":"us/14-cfr-27.674","jurisdiction":"us","citation":"14 CFR 27.674","heading":"Interconnected controls.","body":"Each primary flight control system must provide for safe flight and landing and operate independently after a malfunction, failure, or jam of any auxiliary interconnected control.","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":"fbb883de8de4d6c90af7e25b242058dfd99a2798872cfc3091c0573a167845ae","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.673","next":"us/14-cfr-27.675"},"notice":"GroundRules: Original legal text. Not legal advice."}