{"data":{"id":"us/14-cfr-33.34","jurisdiction":"us","citation":"14 CFR 33.34","heading":"Turbocharger rotors.","body":"Each turbocharger case must be designed and constructed to be able to contain fragments of a compressor or turbine that fails at the highest speed that is obtainable with normal speed control devices inoperative.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES","Subpart C—Design and Construction; Reciprocating Aircraft Engines"],"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":"45e11b85c6a07d5d4893fc441a989bcc32679eb8ce6862ceb3c7b26f18be56f4","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-33.33","next":"us/14-cfr-33.35"},"notice":"GroundRules: Original legal text. Not legal advice."}