{"data":{"id":"us/14-cfr-25.1155","jurisdiction":"us","citation":"14 CFR 25.1155","heading":"Reverse thrust and propeller pitch settings below the flight regime.","body":"Each control for reverse thrust and for propeller pitch settings below the flight regime must have means to prevent its inadvertent operation. The means must have a positive lock or stop at the flight idle position and must require a separate and distinct operation by the crew to displace the control from the flight regime (forward thrust regime for turbojet powered airplanes).","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 25—AIRWORTHINESS STANDARDS: TRANSPORT 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":"12f4d4adf8072d027545c169f1b3dfd0df5427accbd84c86840ca603bde88f16","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-25.1153","next":"us/14-cfr-25.1157"},"notice":"GroundRules: Original legal text. Not legal advice."}