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2023-15178
Airworthiness Directives; Airbus SAS Airplanes
Resumo Rápido
- Número AD
- 2023-15178
- Autoridade
- FAA
- Data de emissão
- 19/07/2023
- Data efetiva
- 23/08/2023
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
19 de julho de 2023
Data Efetiva
23 de agosto de 2023
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (AD) 2013-07-03, que se aplicava a todos os aviões das séries Airbus SAS Modelos A330-200, A330-200 Cargueiro, A330-300, A340-200 e A340-300; e aos aviões Modelos A340-541 e A340-642. A AD 2013-07-03 exigia inspeções repetitivas para degradação dos pinos de pivô do truque e para qualquer trinca e dano dos bucins dos pinos de pivô do trem de pouso principal e central; inspeção dos pinos de pivô do truque afetados para corrosão e trincas do metal base; e reparo ou substituição dos pinos de pivô do truque e bucins dos pinos de pivô, se necessário. Esta AD foi motivada pelo desenvolvimento de uma modificação que aborda a condição insegura e pela determinação de que uma proibição de instalação de peças é necessária. Esta AD continua exigindo certas ações da AD 2013-07-03, adiciona uma modificação opcional que encerraria as inspeções repetitivas e adiciona uma proibição de instalação de peças, conforme especificado na Agência de Segurança da Aviação da União Europeia (EASA), que é incorporada por referência. A FAA está emitindo esta AD para aborda a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2013-07- 03, which applied to all Airbus SAS Model A330-200, A330-200 Freighter, A330-300, A340-200, and A340-300 series airplanes; and Model A340-541 and A340-642 airplanes. AD 2013-07-03 required repetitive inspections for degradation of the bogie pivot pins and for any cracks and damage of the pivot pin bushes of the main and central landing gear; an inspection of the affected bogie pivot pins for corrosion and base metal cracks; and repairing or replacing bogie pivot pins and pivot pin bushes, if necessary. This AD was prompted by development of a modification that address the unsafe condition and a determination that a parts installation prohibition is necessary. This AD continues to require certain actions in AD 2013-07-03, add an optional modification that would terminate the repetitive inspections, and add a parts installation prohibition, as specified in a European Union Aviation Safety Agency (EASA), 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-2023-0011; Project Identifier MCAI-2022-00211-T; Amendment 39-22478; AD 2023-12-19] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2013-07-03, which applied to all Airbus SAS Model A330-200, A330-200 Freighter, A330-300, A340-200, and A340-300 series airplanes; and Model A340-541 and A340-642 airplanes. AD 2013-07-03 required repetitive inspections for degradation of the bogie pivot pins and for any cracks and damage of the pivot pin bushes of the main and central landing gear; an inspection of the affected bogie pivot pins for corrosion and base metal cracks; and repairing or replacing bogie pivot pins and pivot pin bushes, if necessary. This AD was prompted by development of a modification that address the unsafe condition and a determination that a parts installation prohibition is necessary. This AD continues to require certain actions in AD 2013-07-03, add an optional modification that would terminate the repetitive inspections, and add a parts installation prohibition, as specified in a European Union Aviation Safety Agency (EASA), 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 23, 2023. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 23, 2023. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-0011; 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 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. • 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-2023-0011. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206-231-3229; email vladimir.ulyanov@faa.gov. ( printed page 46069) SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2013-07-03, Amendm…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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