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- 2023-10786
2023-10786
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- 2023-10786
- Autoridade
- FAA
- Data de emissão
- 22/05/2023
- Data efetiva
- 26/06/2023
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
22 de maio de 2023
Data Efetiva
26 de junho de 2023
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (AD) para todos os aviões da série Airbus SAS Modelo A318; aviões da série Modelo A319; aviões Modelo A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N e -273N; e aviões da série Modelo A321. Esta AD foi motivada por um relatório indicando que certos elementos sensores do sistema de detecção de superaquecimento (OHDS) instalados em certas posições podem não detectar adequadamente eventos de vazamento de sangria térmica devido a uma falha de qualidade durante o processo de fabricação. Esta AD requer uma inspeção detalhada única de cada peça afetada instalada em uma posição afetada e substituição se necessário, e proíbe a instalação de peças afetadas em posições afetadas, conforme especificado em uma AD da Agência de Segurança da Aviação da União Europeia (EASA), que é incorporada por referência. A FAA está emitindo esta AD para resolver a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for 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. This AD 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. This AD requires a one-time detailed inspection of each affected part installed at an affected position and replacement if necessary, and prohibits the installation of affected parts at affected positions, 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-2022-1491; Project Identifier MCAI-2022-00924-T; Amendment 39-22424; AD 2023-09-01] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 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. This AD 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. This AD requires a one-time detailed inspection of each affected part installed at an affected position and replacement if necessary, and prohibits the installation of affected parts at affected positions, 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 June 26, 2023. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of June 26, 2023. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2022-1491; or in person at Docket Operations between 9 a.m. and ( printed page 32629) 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 EASA material incorporated by reference in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; emailADs@easa.europa.eu; website easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. It is also available in the AD docket at regulations.gov by searching for and locating Docket No. FAA-2022-1491. • For Kidde Aerospace & Defense service information incorporated by reference in this AD, contact Kidde Aerospace & Defense, 4200 Airport Drive NW, Wilson, NC 27896; phone: 252-246-7134; fax: 252-246-7181; email:avionicssupport@collins.com; website kiddeaerospace.com. • 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 in the AD docket atregulations.gov under Docket No. FAA-2022-1491. FOR FURTHER INFORMATION CONTACT: Timothy Dowling, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branc…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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