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2023-15714
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- 2023-15714
- Autoridade
- FAA
- Data de emissão
- 24/07/2023
- Data efetiva
- 08/08/2023
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
24 de julho de 2023
Data Efetiva
08 de agosto de 2023
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (AD) 2022-19-08, que se aplicava a todos os helicópteros Airbus Helicopters modelos SA341G e SA342J. A AD 2022-19-08 foi motivada por um relato de defeitos de fabricação em múltiplas pás de rotor de cauda (TRBs) e exigia inspeção visual de certas pás de rotor de cauda com números de peça específicos quanto à presença de indicação linear e, dependendo dos resultados da inspeção, inspeção por líquido penetrante fluorescente da pá de rotor de cauda e ações corretivas adicionais, se necessário. A AD 2022-19-08 também proibia a instalação de uma pá de rotor de cauda afetada, a menos que determinados requisitos tivessem sido atendidos. Esta AD foi motivada pela determinação de que peças que acumularam mais de 500 horas de voo (HV) desde nova também são afetadas pela condição insegura. Além disso, o tempo de conformidade definido para a inspeção visual da área raiz de cada peça afetada foi determinado como muito rigoroso. Esta AD retém certos requisitos da AD 2022-19-08, inclui todas as pás de rotor de cauda nos requisitos de inspeção e aumenta o tempo de conformidade conforme especificado em uma AD da Agência de Segurança da Aviação da União Europeia (EASA), que está incorporada por referência. A FAA previamente enviou esta AD como uma AD de emergência a todos os proprietários e operadores conhecidos nos EUA desses helicópteros. A FAA está emitindo esta AD para abordar a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2022-19-08 which applied to all Airbus Helicopters Model SA341G and SA342J helicopters. AD 2022-19-08 was prompted by a report of manufacturing defects on multiple tail rotor blades (TRBs) and required visually inspecting certain part-numbered TRBs for the presence of a linear indication, and, depending on the inspection results, fluorescent penetrant inspecting the TRB and further corrective actions if necessary. AD 2022-19-08 also prohibited installing an affected TRB unless certain requirements had been met. This AD was prompted by the determination that parts that have accumulated more than 500 flight hours (FH) since new are also affected by the unsafe condition. In addition, the defined compliance time for the visual inspection of the root area of each affected part was determined to be too strict. This AD retains certain requirements of AD 2022-19-08, includes all TRBs in the inspection requirements, and increases a compliance time 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-2023-1506; Project Identifier MCAI-2023-00784-R; Amendment 39-22512; AD 2023-13-51] • RIN 2120-AA64 ( printed page 47351) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2022-19-08 which applied to all Airbus Helicopters Model SA341G and SA342J helicopters. AD 2022-19-08 was prompted by a report of manufacturing defects on multiple tail rotor blades (TRBs) and required visually inspecting certain part-numbered TRBs for the presence of a linear indication, and, depending on the inspection results, fluorescent penetrant inspecting the TRB and further corrective actions if necessary. AD 2022-19-08 also prohibited installing an affected TRB unless certain requirements had been met. This AD was prompted by the determination that parts that have accumulated more than 500 flight hours (FH) since new are also affected by the unsafe condition. In addition, the defined compliance time for the visual inspection of the root area of each affected part was determined to be too strict. This AD retains certain requirements of AD 2022-19-08, includes all TRBs in the inspection requirements, and increases a compliance time 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. DATES: This AD is effective August 8, 2023. Emergency AD 2023-13-51, issued on June 27, 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 August 8, 2023. The FAA must receive comments on this AD by September 7, 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. Material Incorporated by Reference: • For EASA material incorporated by reference 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 the FAA, call (817) 222-5110. Service information that is incorporat…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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