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- 2025-02039
2025-02039
Diretivas de Aeronavegabilidade; Aeronaves Airbus SAS
Resumo Rápido
- Número AD
- 2025-02039
- Autoridade
- FAA
- Data de emissão
- 31/01/2025
- Data efetiva
- 18/02/2025
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
31 de janeiro de 2025
Data Efetiva
18 de fevereiro de 2025
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2023-09-01, que se aplicava a todos os aviões da série Model A318 da Airbus SAS; aviões da série Model A319; aviões Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N e -273N; e aviões da série Model A321. A DA 2023-09-01 foi motivada por um relato de que certos elementos sensores do sistema de detecção de superaquecimento (SDSA) instalados em certas posições podem não detectar adequadamente eventos de vazamento de ar de sangria térmica devido a uma falha de qualidade durante o processo de fabricação. A DA 2023-09-01 exigia uma inspeção detalhada única de cada peça afetada instalada em uma posição afetada e substituição se necessária e proibia a instalação de peças afetadas em posições afetadas. Desde que a FAA emitiu a DA 2023-09-01, um novo modelo de avião (A321-253NY) foi certificado pela EASA, no qual peças afetadas podem ser instaladas em serviço. Esta DA continua exigindo as ações da DA 2023-09-01 e revisa a aplicabilidade para incluir aviões Model A321-253NY, conforme especificado em uma DA da Agência de Segurança da Aviação da União Europeia (EASA), que é incorporada por referência. A FAA está emitindo esta DA para abordar a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2023-09- 01, which applied to all Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320-211, -212, -214, -216, -231, -232, - 233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes; and Model A321 series airplanes. AD 2023-09-01 was prompted by a report that certain overheat detection system (OHDS) sensing elements installed at certain positions might not properly detect thermal bleed leak events due to a quality escape during the manufacturing process. AD 2023-09-01 required a one-time detailed inspection of each affected part installed at an affected position and replacement if necessary and prohibited the installation of affected parts at affected positions. Since the FAA issued AD 2023-09-01, a new airplane model (A321-253NY) has been certified by EASA, on which affected parts could be installed in service. This AD continues to require the actions in AD 2023-09-01, and revises the applicability to include Model A321-253NY airplanes, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. 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-2024-2715; Project Identifier MCAI-2024-00621-T; Amendment 39-22919; AD 2024-26-04] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-09-01, which applied to all Airbus SAS Model A318 series airplanes; Model A319 series airplanes; Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes; and Model A321 series airplanes. AD 2023-09-01 was prompted by a report that certain overheat detection system (OHDS) sensing elements installed at certain positions might not properly detect thermal bleed leak events due to a quality escape during the manufacturing process. AD 2023-09-01 required a one-time detailed inspection of each affected part installed at an affected position and replacement if necessary and prohibited the installation of affected parts at affected positions. Since the FAA issued AD 2023-09-01, a new airplane model (A321-253NY) has been certified by EASA, on which affected parts could be installed in service. This AD continues to require the actions in AD 2023-09-01, and revises the applicability to include Model A321-253NY airplanes, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective February 18, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of February 18, 2025. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of June 26, 2023 (88 FR 32628, May 22, 2023). The FAA must receive comments on this AD by March 17, 2025. 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-2024-2715; 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 EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; emailADs@easa.europa.eu; website …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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