{"data":{"id":"us/14-cfr-33.82","jurisdiction":"us","citation":"14 CFR 33.82","heading":"General.","body":"Before each endurance test required by this subpart, the adjustment setting and functioning characteristic of each component having an adjustment setting and a functioning characteristic that can be established independent of installation on the engine must be established and recorded.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES","Subpart F—Block Tests; Turbine 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":"ab05781bd051a1bfb0b09832da51fb450fe1c8024cabb4ea51421063ee72acd4","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-33.81","next":"us/14-cfr-33.83"},"notice":"GroundRules: Original legal text. Not legal advice."}