{"data":{"id":"us/14-cfr-35.16","jurisdiction":"us","citation":"14 CFR 35.16","heading":"Propeller critical parts.","body":"The integrity of each propeller critical part identified by the safety analysis required by § 35.15 must be established by:\n(a) A defined engineering process for ensuring the integrity of the propeller critical part throughout its service life,\n(b) A defined manufacturing process that identifies the requirements to consistently produce the propeller critical part as required by the engineering process, and\n(c) A defined service management process that identifies the continued airworthiness requirements of the propeller critical part as required by the engineering process.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 35—AIRWORTHINESS STANDARDS: PROPELLERS","Subpart B—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":"5f46b42434fff614c741c14a50a8bbd02041450c355c035ec00b5221610bdd4e","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-35.15","next":"us/14-cfr-35.17"},"notice":"GroundRules: Original legal text. Not legal advice."}