{"abstract":"The FAA is superseding Airworthiness Directive (AD) 2007-06-11 (AD 2007-06-11) for certain SOCATA (type certificate now held by DAHER AEROSPACE) Model TBM 700 airplanes. AD 2007-06-11 required repetitively inspecting the vertical stabilizer attachment fittings and bolts for cracks or corrosion, and, if necessary, repairing or replacing the damaged part and then applying a corrosion protection reinforcement. Since the FAA issued AD 2007-06-11, the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, superseded the previous Direction generale de l'aviation civile (DGAC) France AD to introduce new service information providing instructions for installing new vertical stabilizer attachment fittings having improved corrosion resistant material as an optional terminating action for the repetitive inspections. This AD retains the requirements of AD 2007-06-11 and includes a new optional terminating action for the repetitive inspections. The FAA is issuing this AD to address the unsafe condition on these products.","action":"Final rule.","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"body_html_url":"https://www.federalregister.gov/documents/full_text/html/2026/01/08/2026-00162.html","cfr_references":[{"chapter":null,"citation_url":null,"part":39,"title":14}],"citation":"91 FR 555","comment_url":null,"comments_close_on":null,"correction_of":null,"corrections":[],"dates":"This AD is effective February 12, 2026.","disposition_notes":null,"docket_ids":["Docket No. FAA-2025-2265","Project Identifier MCAI-2024-00714-A","Amendment 39-23224","AD 2025-26-02"],"dockets":[{"supporting_documents":[{"title":"U.S. DOT/FAA - Supplemental AD Documents","document_id":"FAA-2025-2265-0012"},{"title":"U.S. DOT/FAA - Supplemental AD Documents","document_id":"FAA-2025-2265-0002"}],"agency_name":"FAA","documents":[{"comment_count":0,"comment_start_date":"2026-01-08","updated_at":"2026-01-08T08:56:19.955-05:00","comment_url":"https://www.regulations.gov/commenton/FAA-2025-2265-0011","allow_late_comments":false,"id":"FAA-2025-2265-0011","comment_end_date":null,"regulations_dot_gov_open_for_comment":false}],"supporting_documents_count":2,"id":"FAA-2025-2265","title":"MCAI-2024-00714-A; DAHER AEROSPACE (previously SOCATA) Model TBM 700 airplanes; Vertical Stabilizer Attachment Fittings – Inspection / Modification"}],"document_number":"2026-00162","effective_on":"2026-02-12","end_page":558,"executive_order_notes":null,"executive_order_number":null,"explanation":null,"full_text_xml_url":"https://www.federalregister.gov/documents/full_text/xml/2026/01/08/2026-00162.xml","html_url":"https://www.federalregister.gov/documents/2026/01/08/2026-00162/airworthiness-directives-daher-aerospace-type-certificate-previously-held-by-socata-airplanes","images":{},"images_metadata":{},"json_url":"https://www.federalregister.gov/api/v1/documents/2026-00162?publication_date=2026-01-08","mods_url":"https://www.govinfo.gov/metadata/granule/FR-2026-01-08/2026-00162/mods.xml","not_received_for_publication":null,"page_length":4,"page_views":{"count":167,"last_updated":"2026-04-04 16:15:04 -0400"},"pdf_url":"https://www.govinfo.gov/content/pkg/FR-2026-01-08/pdf/2026-00162.pdf","presidential_document_number":null,"proclamation_number":null,"public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2026-00162.pdf?1767793514","publication_date":"2026-01-08","raw_text_url":"https://www.federalregister.gov/documents/full_text/text/2026/01/08/2026-00162.txt","regulation_id_number_info":{"2120-AA64":{"issue":"202504","html_url":"https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives","title":"Airworthiness Directives","xml_url":"http://www.reginfo.gov/public/do/eAgendaViewRule?pubId=202504&RIN=2120-AA64&operation=OPERATION_EXPORT_XML","priority_category":"Routine and Frequent"}},"regulation_id_numbers":["2120-AA64"],"regulations_dot_gov_info":{"supporting_documents":[{"title":"U.S. DOT/FAA - Supplemental AD Documents","document_id":"FAA-2025-2265-0012"},{"title":"U.S. DOT/FAA - Supplemental AD Documents","document_id":"FAA-2025-2265-0002"}],"regulatory_plan":{"html_url":"https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives","title":"Airworthiness Directives"},"comments_count":0,"agency_id":"FAA","comments_url":"https://www.regulations.gov/docketBrowser?rpp=50&so=DESC&sb=postedDate&po=0&dct=PS&D=FAA-2025-2265","supporting_documents_count":2,"docket_id":"FAA-2025-2265","document_id":"FAA-2025-2265-0011","regulation_id_number":"2120-AA64","title":"MCAI-2024-00714-A; DAHER AEROSPACE (previously SOCATA) Model TBM 700 airplanes; Vertical Stabilizer Attachment Fittings – Inspection / Modification","checked_regulationsdotgov_at":"2026-01-09T18:55:06Z"},"regulations_dot_gov_url":null,"significant":false,"signing_date":null,"start_page":555,"subtype":null,"title":"Airworthiness Directives; DAHER AEROSPACE (Type Certificate Previously Held by SOCATA) Airplanes","toc_doc":"DAHER AEROSPACE (Type Certificate previously held by SOCATA) Airplanes","toc_subject":"Airworthiness Directives","topics":["Air transportation","Aircraft","Aviation safety","Incorporation by reference","Safety"],"type":"Rule","volume":91}