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- FAA-2026-07183
FAA-2026-07183
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- FAA-2026-07183
- Autoridade
- FAA
- Data de emissão
- 14/04/2026
- Data efetiva
- 29/04/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de abril de 2026
Data Efetiva
29 de abril de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (DA) para certos aviões Airbus SAS Modelo A350-1041. Esta DA foi motivada por um relatório de desalinhamento entre um determinado eixo de flap e o dispositivo de retenção devido à instalação incorreta do suporte do dispositivo de retenção. Esta DA exige uma inspeção das partes afetadas e as ações corretivas aplicáveis. A FAA está emitindo esta DA para resolver a condição insegura destes produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-1041 airplanes. This AD was prompted by a report of a misalignment between a certain flap shaft and the catcher due to incorrect installation of the bracket supporting the catcher. This AD requires an inspection of affected parts and applicable corrective actions. 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-2026-3478; Project Identifier MCAI-2025-00934-T; Amendment 39-23307; AD 2026-07-11] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A350-1041 airplanes. This AD was prompted by a report of a misalignment between a certain flap shaft and the catcher due to incorrect installation of the bracket supporting the catcher. This AD requires an inspection of affected parts and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 29, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 29, 2026. The FAA must receive comments on this AD by May 29, 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-2026-3478; 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-2026-3478. FOR FURTHER INFORMATION CONTACT: Nicholas Benson, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3647; email: Nicholas.H.Benson@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written data, views, or…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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