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- 2023-22856
2023-22856
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- 2023-22856
- Autoridade
- FAA
- Data de emissão
- 16/10/2023
- Data efetiva
- 31/10/2023
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
16 de outubro de 2023
Data Efetiva
31 de outubro de 2023
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova Diretiva de Aeronavegabilidade (AD) para helicópteros Airbus Helicopters Modelo AS332C, AS332C1, AS332L, AS332L1, AS332L2 e SA330J. Esta AD foi motivada por um relato de três placas retentoras de bucha de placa oscilante do rotor principal recém-fornecidas com diâmetros internos superdimensionados. Esta AD requer a realização de uma inspeção única para medir o diâmetro interno das placas retentoras de bucha afetadas e, dependendo dos resultados, realizar uma inspeção adicional, substituir placas retentoras de bucha não-conformes ou realizar ação corretiva adicional, conforme especificado em uma AD da Agência de Segurança da Aviação da União Europeia (EASA), que é incorporada por referência. A FAA enviou previamente esta AD como uma AD emergencial a todos os proprietários e operadores conhecidos destes helicópteros nos EUA. A FAA está emitindo esta AD para tratar a condição insegura nestes produtos.
The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and SA330J helicopters. This AD was prompted by a report of three newly supplied main rotor swashplate bushing retaining plates with oversized internal diameters. This AD requires accomplishing a one-time inspection to measure the internal diameter of affected bushing retaining plates and depending on the results, accomplishing an additional inspection, replacing non-conforming bushing retaining plates, or accomplishing additional corrective action, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA previously sent this AD as an emergency AD to all known U.S. owners and operators of these helicopters. 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-2023-1998; Project Identifier MCAI-2023-01045-R; Amendment 39-22572; AD 2023-20-51] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, and SA330J helicopters. This AD was prompted by a report of three newly supplied main rotor swashplate bushing retaining plates with oversized internal diameters. This AD requires accomplishing a one-time inspection to measure the internal diameter of affected bushing retaining plates and depending on the results, accomplishing an additional inspection, replacing non-conforming bushing retaining plates, or accomplishing additional corrective action, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA previously sent this AD as an emergency AD to all known U.S. owners and operators of these helicopters. The FAA is issuing this AD to address the unsafe condition on these products. ( printed page 71284) DATES: This AD is effective October 31, 2023. Emergency AD 2023-20-51, issued on October 2, 2023, which contained the requirements of this amendment, was effective with actual notice. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 31, 2023. The FAA must receive comments on this AD by November 30, 2023. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: (202) 493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-1998; 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 listed above. Material Incorporated by Reference: • For EASA material identified in this final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; emailADs@easa.europa.eu; internet easa.europa.eu. You may find the EASA material on the EASA website at ad.easa.europa.eu. • You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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