{"database": "openregs", "table": "cfr_sections", "rows": [["14:14:1.0.1.3.15.3.169.19", 14, "Aeronautics and Space", "I", "C", "27", "PART 27\u2014AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT", "C", "Subpart C\u2014Strength Requirements", "27.473", "\u00a7 27.473 Ground loading conditions and assumptions.", "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.", "[Amdt. 27-2, 33 FR 963, Jan. 26, 1968]", "(a) For specified landing conditions, a design maximum weight must be used that is not less than the maximum weight. A rotor lift may be assumed to act through the center of gravity throughout the landing impact. This lift may not exceed two-thirds of the design maximum weight.\n\n(b) Unless otherwise prescribed, for each specified landing condition, the rotorcraft must be designed for a limit load factor of not less than the limit inertia load factor substantiated under \u00a7 27.725."]], "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": ["14:14:1.0.1.3.15.3.169.19"], "units": {}, "query_ms": 0.22620498202741146, "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"}