{"data":{"id":"us/14-cfr-33.11","jurisdiction":"us","citation":"14 CFR 33.11","heading":"Applicability.","body":"This subpart prescribes the general design and construction requirements for reciprocating and turbine aircraft engines.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES","Subpart B—Design and Construction; General"],"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":"deb53d9304dc374169bc3574f2d9da7bfb5b08c8c882ea15ea0f1a0deebc3842","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-33.8","next":"us/14-cfr-33.13"},"notice":"GroundRules: Original legal text. Not legal advice."}