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- 2021-22293
2021-22293
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- 2021-22293
- Autoridade
- FAA
- Data de emissão
- 14/10/2021
- Data efetiva
- 18/11/2021
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
14 de outubro de 2021
Data Efetiva
18 de novembro de 2021
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (AD) 2019-19-06, que se aplicava a determinados aviões Airbus SAS modelo A330-202, -243, -243F, -302, -323 e -343. A AD 2019-19-06 exigia uma inspeção para determinar o número de peça e número de série dos atuadores rotativos engrenados de slat (SGRA), e substituição de cada SGRA afetado por uma peça em condições de aeronavegabilidade. Esta AD continua exigindo a substituição de cada SGRA afetado por uma peça em condições de aeronavegabilidade, amplia a aplicabilidade para incluir todos os aviões nos quais a peça afetada possa estar instalada, e também proíbe a instalação de uma peça afetada, conforme especificado em uma AD da Agência de Segurança da Aviação da União Europeia (EASA), que é incorporada por referência. Esta AD foi motivada por um relato de que trincas foram encontradas nos anéis de engrenagem dos SGRA devido a uma alteração no processo de fabricação e testes não destrutivos pós-produção inadequados para detecção potencial de trincas, e uma determinação de que os requisitos da AD 2019-19-06 podem não garantir a remoção permanente do serviço dos SGRA afetados. A FAA está emitindo esta AD para abordar a condição insegura desses produtos.
The FAA is superseding Airworthiness Directive (AD) 2019-19- 06, which applied to certain Airbus SAS Model A330-202, -243, -243F, - 302, -323, and -343 airplanes. AD 2019-19-06 required an inspection to determine the part number and serial number of the slat geared rotary actuators (SGRAs), and replacement of each affected SGRA with a serviceable part. This AD continues to require replacement of each affected SGRA with a serviceable part, expands the applicability to include all airplanes on which the affected part may be installed, and also prohibits installation of an affected part; as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by a report that cracks have been found within the ring gears of the SGRAs due to a change in the manufacturing process and inadequate post-production non-destructive testing for potential cracking, and a determination that the requirements of AD 2019-19-06 may not ensure the permanent removal from service of affected SGRAs. 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-2021-0261; Project Identifier MCAI-2020-01502-T; Amendment 39-21753; AD 2021-20-15] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-19-06, which applied to certain Airbus SAS Model A330-202, -243, -243F, -302, -323, and -343 airplanes. AD 2019-19-06 required an inspection to determine the part number and serial number of the slat geared rotary actuators (SGRAs), and replacement of each affected SGRA with a serviceable part. This AD continues to require replacement of each affected SGRA with a serviceable part, expands the applicability to include all airplanes on which the affected part may be installed, and also prohibits installation of an affected part; as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD was prompted by a report that cracks have been found within the ring gears of the SGRAs due to a change in the manufacturing process and inadequate post-production non-destructive testing for potential cracking, and a determination that the requirements of AD 2019-19-06 may not ensure the permanent removal from service of affected SGRAs. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 18, 2021. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 18, 2021. 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 IBR material on the EASA website at https://ad.easa.europa.eu. You may view this IBR 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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0261. Examining the AD Docket You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0261; 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, 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, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229; email vladimir.ulyanov@faa.gov. SUPPLEMENTARY INFORMATION: ( printed page 57028) Background EASA, which is the Techni…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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