{"data":{"id":"us/14-cfr-23.2420","jurisdiction":"us","citation":"14 CFR 23.2420","heading":"Reversing systems.","body":"Each reversing system must be designed so that—\n(a) No unsafe condition will result during normal operation of the system; and\n(b) The airplane is capable of continued safe flight and landing after any single failure, likely combination of failures, or malfunction of the reversing system.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 23—AIRWORTHINESS STANDARDS: NORMAL CATEGORY AIRPLANES","Subpart E—Powerplant"],"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":"204ddb2e1c2d28833125371fe9fa242f6e2b8a3dc803fbe2cef86403c2c0c53f","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-23.2415","next":"us/14-cfr-23.2425"},"notice":"GroundRules: Original legal text. Not legal advice."}