{"database": "openregs", "table": "cfr_sections", "rows": [["14:14:1.0.1.3.15.4.176.19", 14, "Aeronautics and Space", "I", "C", "27", "PART 27\u2014AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT", "D", "Subpart D\u2014Design and Construction", "27.671", "\u00a7 27.671 General.", "FAA", "49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704.", "Docket No. 5074, 29 FR 15695, Nov. 24, 1964, unless otherwise noted.", "", "(a) Each control and control system must operate with the ease, smoothness, and positiveness appropriate to its function.\n\n(b) Each element of each flight control system must be designed, or distinctively and permanently marked, to minimize the probability of any incorrect assembly that could result in the malfunction of the system."]], "columns": ["section_id", "title_number", "title_name", "chapter", "subchapter", "part_number", "part_name", "subpart", "subpart_name", "section_number", "section_heading", "agency", "authority", "source_citation", "amendment_citations", "full_text"], "primary_keys": ["section_id"], "primary_key_values": ["14:14:1.0.1.3.15.4.176.19"], "units": {}, "query_ms": 0.23118394892662764, "source": "Federal Register API & Regulations.gov API", "source_url": "https://www.federalregister.gov/developers/api/v1", "license": "Public Domain (U.S. Government data)", "license_url": "https://www.regulations.gov/faq"}