{"data":{"id":"us/14-cfr-27.1527","jurisdiction":"us","citation":"14 CFR 27.1527","heading":"Maximum operating altitude.","body":"The maximum altitude up to which operation is allowed, as limited by flight, structural, powerplant, functional, or equipment characteristics, must be established.","path":["Title 14—Aeronautics and Space","CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION","SUBCHAPTER C—AIRCRAFT","PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT","Subpart G—Operating Limitations and Information"],"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":"3b5fc3477c8535e7fb492b998afb351eaef979063f3d1d36581575bd424cac53","source_id":"us-cfr","stale":true,"prev":"us/14-cfr-27.1525","next":"us/14-cfr-27.1529"},"notice":"GroundRules: Original legal text. Not legal advice."}