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- 2023-27681
2023-27681
Diretivas de Aeronavegabilidade; Aeronaves Airbus SAS
Resumo Rápido
- Número AD
- 2023-27681
- Autoridade
- FAA
- Data de emissão
- 19/12/2023
- Data efetiva
- 23/01/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
19 de dezembro de 2023
Data Efetiva
23 de janeiro de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (AD) 2019-12-07, que se aplicava a todos os aviões Airbus SAS modelo A318-111, -112, -121 e -122; modelo A319-111, -112, -113, -114, -115, -131, -132 e -133; modelo A320-211, -212, -214, -216, -231, -232 e -233; e modelo A321-111, -112, -131, -211, -212, -213, -231 e -232. A AD 2019-12-07 exigia a substituição de ambos os amortecedores de choque do trem de pouso principal (MLG), uma identificação dos tubos deslizantes do MLG afetados, inspeção das placas de crômio e eixos dos tubos deslizantes afetados quanto a danos e substituição do tubo deslizante se necessário. A AD 2019-12-07 também exigia inspeções repetitivas dos tubos deslizantes do MLG afetados quanto a trincas, substituição dos tubos deslizantes do MLG trincados e eventual substituição de cada tubo deslizante do MLG afetado. Esta AD continua a exigir as ações especificadas na AD 2019-12-07 e exige inspeções repetitivas de tubos deslizantes adicionais do MLG, substituição se necessário e eventual substituição dos tubos deslizantes adicionais do MLG. Esta AD também estende o intervalo de inspeção repetitiva. Esta AD também proíbe a instalação de peças afetadas sob certas condições. Esta AD foi motivada pela determinação da FAA de que tubos deslizantes adicionais do MLG são afetados pela condição insegura e que o intervalo de inspeção repetitiva pode ser estendido. A FAA está emitindo esta AD para resolver a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2019-12- 07, which applied to all Airbus SAS Model A318-111, -112, -121, and - 122 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. AD 2019-12-07 required replacement of both main landing gear (MLG) shock absorbers, an identification of affected MLG sliding tubes; inspection of affected chromium plates and sliding tube axles for damage; and replacement of the sliding tube if necessary. AD 2019- 12-07 also required repetitive inspections of affected MLG sliding tubes for cracking, replacement of cracked MLG sliding tubes, and eventual replacement of each affected MLG sliding tube. This AD continues to require the actions specified in AD 2019-12-07 and requires repetitive inspections of additional MLG sliding tubes, replacement if necessary, and eventual replacement of the additional MLG sliding tubes. This AD also extends the repetitive inspection interval. This AD also prohibits the installation of affected parts under certain conditions. This AD was prompted by the FAA's determination that additional MLG sliding tubes are affected by the unsafe condition and that the repetitive inspection interval may be extended. 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-2023-1645; Project Identifier MCAI-2022-01296-T; Amendment 39-22613; AD 2023-23-11] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-12-07, which applied to all Airbus SAS Model A318-111, -112, -121, and -122 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. AD 2019-12-07 required replacement of both main landing gear (MLG) shock absorbers, an identification of affected MLG sliding tubes; inspection of affected chromium plates and sliding tube axles for damage; and replacement of the sliding tube if necessary. AD 2019-12-07 also required repetitive inspections of affected MLG sliding tubes for cracking, replacement of cracked MLG sliding tubes, and eventual replacement of each affected MLG sliding tube. This AD continues to require the actions specified in AD 2019-12-07 and requires repetitive inspections of additional MLG sliding tubes, replacement if necessary, and eventual replacement of the additional MLG sliding tubes. This AD also extends the repetitive inspection interval. This AD also prohibits the installation of affected parts under certain conditions. This AD was prompted by the FAA's determination that additional MLG sliding tubes are affected by the unsafe condition and ( printed page 87656) that the repetitive inspection interval may be extended. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 23, 2024. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of January 23, 2024. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of August 1, 2019 (84 FR 30579, June 27, 2019). The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of February 22, 2017 (82 FR 5362, January 18, 2017). The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of June 29, 2007 (72 FR 29241, May 25, 2007). The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of June 23, 2004 (69 FR 31867, June 8, 2004). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-1645; 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 Airbus service information identified in this final rule, contact Airbus SAS, Airworthi…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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