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- FAA-2026-04830
FAA-2026-04830
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- FAA-2026-04830
- Autoridade
- FAA
- Data de emissão
- 12/03/2026
- Data efetiva
- 27/03/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
12 de março de 2026
Data Efetiva
27 de março de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (DA) para certos aviões Airbus SAS Modelo A350-941. Esta DA foi motivada por um relato de não conformidade no processo de serialização de certos pinos de fusível e pinos de retenção instalados na fixação do bloco de trunnion do trem de pouso principal (TPP), resultando em uma combinação não única de número de peça e número de série que poderia levar à falta de rastreabilidade. Esta DA requer a execução de uma verificação para identificar o número de peça e número de série das peças afetadas. Esta DA também requer a inspeção do pino de retenção da fixação do bloco de trunnion do TPP afetado e dos pinos de fusível, registrando a combinação de número de ordem de trabalho e número de série original como o novo número de série, e atualizando os registros de manutenção, conforme aplicável. A FAA está emitindo esta DA para resolver a condição insegura desses produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 airplanes. This AD was prompted by a report of a non-conformity in the serialization process of certain fuse pins and retaining pins installed in the main landing gear (MLG) trunnion block attachment, resulting in a non-unique combination of part number and serial number that could lead to a lack of traceability. This AD requires doing a check to identify the part number and serial number of the affected parts. This AD also requires inspecting the affected MLG trunnion block attachment retaining pin and fuse pins, recording the combination of work order number and original serial number as the new serial number, and updating the maintenance records, as applicable. The FAA is issuing this AD to address the unsafe condition on these products.Texto Completo da Diretiva
Expandir texto completo (Federal Register)Texto completo (Federal Register)
Document Headings Document headings vary by document type but may contain the following: • the agency or agencies that issued and signed a document • the number of the CFR title and the number of each part the document amends, proposes to amend, or is directly related to • the agency docket number / agency internal file number • the RIN which identifies each regulatory action listed in the Unified Agenda of Federal Regulatory and Deregulatory Actions See the Document Drafting Handbook for more details. Department of Transportation Federal Aviation Administration • 14 CFR Part 39 • [Docket No. FAA-2026-2291; Project Identifier MCAI-2026-00074-T; Amendment 39-23285; AD 2026-05-12] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ( printed page 12056) ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 airplanes. This AD was prompted by a report of a non-conformity in the serialization process of certain fuse pins and retaining pins installed in the main landing gear (MLG) trunnion block attachment, resulting in a non-unique combination of part number and serial number that could lead to a lack of traceability. This AD requires doing a check to identify the part number and serial number of the affected parts. This AD also requires inspecting the affected MLG trunnion block attachment retaining pin and fuse pins, recording the combination of work order number and original serial number as the new serial number, and updating the maintenance records, as applicable. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective March 27, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 27, 2026. The FAA must receive comments on this AD by April 27, 2026. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: 202-493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-2291; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For European Union Aviation Safety Agency (EASA) material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; emailADs@easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available atregulations.gov under Docket No. FAA-2026-2291. …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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