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2022-14969
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- 2022-14969
- Autoridade
- FAA
- Data de emissão
- 14/07/2022
- Data efetiva
- 18/08/2022
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de julho de 2022
Data Efetiva
18 de agosto de 2022
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2019-03-25, que se aplicava a certos aviões da série Airbus SAS Modelo A318; modelos A319-111, -112, -113, -114, -115, -131, -132 e -133; modelos A320-211, -212, -214, -216, -231, -232 e -233; e modelos A321-111, -112, -131, -211, -212, -213, -231 e -232. A DA 2019-03-25 exigia inspeções repetitivas dos reforçadores e painéis inferiores da caixa alar central e externa em uma determinada junção nos lados esquerdo e direito para qualquer trinca, com reparo se necessário. A DA 2019-03-25 também fornecia uma modificação opcional, que terminaria as inspeções repetitivas. Esta DA foi motivada pela determinação de que, para certos aviões, o tempo de conformidade para a inspeção inicial é inadequado e deve ser revisado. Esta DA continua a exigir as ações especificadas na DA 2019-03-25 com prazos de conformidade revisados para certos aviões e ações adicionais para certos aviões, e amplia a aplicabilidade, conforme especificado em uma Diretiva de Aeronavegabilidade 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 superseding Airworthiness Directive (AD) 2019-03- 25, which applied to certain Airbus SAS Model 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. AD 2019-03-25 required repetitive inspections of the center and outer wing box lower stiffeners and panels at a certain junction on the left- and right-hand sides for any cracking, and repair if necessary. AD 2019-03-25 also provided an optional modification, which would terminate the repetitive inspections. This AD was prompted by a determination that, for certain airplanes, the compliance time for the initial inspection is inadequate and must be revised. This AD continues to require the actions specified in AD 2019-03-25 with revised compliance times for certain airplanes and additional actions for certain airplanes, and expands the applicability, as specified in a European 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-2022-0454; Project Identifier MCAI-2021-01124-T; Amendment 39-22106; AD 2022-14-01] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-03-25, which applied to certain Airbus SAS Model 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. AD 2019-03-25 required repetitive inspections of the center and outer wing box lower stiffeners and panels at a certain junction on the left- and right-hand sides for any cracking, and repair if necessary. AD 2019-03-25 also provided an optional modification, which would terminate the repetitive inspections. This AD was prompted by a determination that, for certain airplanes, the compliance time for the initial inspection is inadequate and must be revised. This AD continues to require the actions specified in AD 2019-03-25 with revised compliance times for certain airplanes and additional actions for certain airplanes, and expands the applicability, as specified in a European 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 August 18, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 18, 2022. ADDRESSES: For material incorporated by reference (IBR) in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this material on the EASA website at https://ad.easa.europa.eu. You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South ( printed page 42064) 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 at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0454. Examining the AD Docket You may examine the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0454; 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. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3223; email Vladimir.Ulyanov@faa.gov. SUPPLEMENTARY IN…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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