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- FAA-2026-10801
FAA-2026-10801
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- FAA-2026-10801
- Autoridade
- FAA
- Data de emissão
- 29/05/2026
- Data efetiva
- 06/07/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
29 de maio de 2026
Data Efetiva
06 de julho de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (DA) para determinados aviões Airbus SAS série Model A318; aviões Model A319-111, -112, -113, -114, -115, -131, -132 e -133; aviões Model A320-211, -212, -214, -216, -231, -232 e -233; e aviões Model A321-111, -112, -131, -211, -212, -213, -231 e -232. Esta DA foi originada por relatos de parafusos quebrados nas conexões dos trilhos de assentos de determinadas estruturas. Esta DA requer a substituição dos bucins de nylon por bucins de bronze nas áreas afetadas e também proíbe a instalação de peças afetadas nessas áreas. A FAA está emitindo esta DA para corrigir a condição insegura nestes produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, - 113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, - 131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by reports of broken bolts in seat rail connections of certain frames. This AD requires replacement of the nylon bushes with bronze bushes in the affected areas and also prohibits the installation of affected parts in those areas. 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-2026-2286; Project Identifier MCAI-2025-01556-T; Amendment 39-23357; AD 2026-10-17] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by reports of broken bolts in seat rail connections of certain frames. This AD requires replacement of the nylon bushes with bronze bushes in the affected areas and also prohibits the installation of affected parts in those areas. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective July 6, 2026. ( printed page 31888) The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 6, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-2286; 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 address for Docket Operations is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. 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-2026-2286. FOR FURTHER INFORMATION CONTACT: Camille L. Seay, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone 817-222-5149; email Camille.L.Seay@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. The NPRM was published in the Federal Register on March 10, 2026 (91 FR 11478). The NPRM was prompted by EASA AD 2025-0207R1, dated October 30, 2025 (EASA AD…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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