{"database": "openregs", "table": "federal_register", "rows": [["03-31849", "Airworthiness Directives; Agusta S.p.A. Model A109E Helicopters", "Rule", "This amendment adopts a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E helicopters. This action requires certain inspections of the rod-end of the main rotor head damper for freedom of movement, and depending on the torque required to move the rod-end, either further inspection for a crack or replacing the rod- end. This amendment is prompted by reports of rod-end fractures due to fatigue failure resulting in increased helicopter vibrations. This condition, if not corrected, could result in failure of the rod-end, extreme vibrations, and a subsequent forced landing or loss of control of the helicopter.", "2003-12-31", 2003, 12, "https://www.federalregister.gov/documents/2003/12/31/03-31849/airworthiness-directives-agusta-spa-model-a109e-helicopters", "https://www.govinfo.gov/content/pkg/FR-2003-12-31/pdf/03-31849.pdf", "Transportation Department; Federal Aviation Administration", "492,159", "This amendment adopts a new airworthiness directive (AD) for Agusta S.p.A. (Agusta) Model A109E helicopters. This action requires certain inspections of the rod-end of the main rotor head damper for freedom of movement, and depending on the torque...", "2120-AA64"]], "columns": ["document_number", "title", "type", "abstract", "publication_date", "pub_year", "pub_month", "html_url", "pdf_url", "agency_names", "agency_ids", "excerpts", "regulation_id_numbers"], "primary_keys": ["document_number"], "primary_key_values": ["03-31849"], "units": {}, "query_ms": 5.620002000796376, "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"}