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- FAA-R1-2025-04334
FAA-R1-2025-04334
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- FAA-R1-2025-04334
- Autoridade
- FAA
- Data de emissão
- 01/04/2025
- Data efetiva
- 22/04/2025
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
01 de abril de 2025
Data Efetiva
22 de abril de 2025
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (DA) para todos os aviões Airbus SAS modelo A350-941 e A350-1041. Esta DA foi motivada por um relatório indicando que os inversores de empuxo e os cobertores térmicos do pilone foram encontrados danificados devido a vazamento de ar do trocador pré-resfriador (TPR). Esta DA requer testes repetitivos do TPR para vazamento de ar e relatório dos resultados, e, dependendo dos achados, inspeção dos cobertores térmicos quanto a danos e substituição do TPR, conforme especificado em uma DA da Agência Europeia de Segurança da Aviação (EASA), que é incorporada por referência. A FAA está emitindo esta DA para abordar a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A350-941 and A350-1041 airplanes. This AD was prompted by a report indicating that the thrust reverser and pylon thermal blankets were found damaged due to air leaking from the pre-cooler exchanger (PCE). This AD requires repetitively testing the PCE for air leaks and reporting the results, and, depending on findings, inspecting the thermal blankets for damage and replacing the PCE, 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-2024-1701; Project Identifier MCAI-2024-00153-T; Amendment 39-22986; AD 2025-05-14] • RIN 2120-AA64 ( printed page 14331) Editorial Note Editorial Note: Rule document 2024-04334 originally published on pages 12449-12452 in the issue of Tuesday, March 18, 2025. In that publication, on page 12449, in the second column, in the DATES section, in the first through fourth lines, “INSERT DATE 35 DAYS AFTER DATE OF PUBLICATION IN THE Federal Register ]” should read “April 22, 2025”. The rule is republished here corrected and in its entirety. AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A350-941 and A350-1041 airplanes. This AD was prompted by a report indicating that the thrust reverser and pylon thermal blankets were found damaged due to air leaking from the pre-cooler exchanger (PCE). This AD requires repetitively testing the PCE for air leaks and reporting the results, and, depending on findings, inspecting the thermal blankets for damage and replacing the PCE, 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 April 22, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 22, 2025. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-1701; 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 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 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-2024-1701. FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3225; email: dan.rodina@faa.gov. SUPPLEMENTARY INFORMATION: Background Th…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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