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2024-24365
Diretivas de Aeronavegabilidade; Motores Safran Helicopter Engines, S.A. (Certificado de Tipo Anteriormente Mantido pela Turbomeca, S.A.)
Resumo Rápido
- Número AD
- 2024-24365
- Autoridade
- FAA
- Data de emissão
- 22/10/2024
- Data efetiva
- 26/11/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
22 de outubro de 2024
Data Efetiva
26 de novembro de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova Diretiva de Aeronavegabilidade (DA) para todos os motores Safran Helicopter Engines, S.A. (Safran) (certificado de tipo anteriormente mantido pela Turbomeca, S.A.) modelos Makila 1A, Makila 1A1 e Makila 1A2. Esta DA é motivada pela determinação de que a vida útil acumulada de certas peças críticas foi subestimada. Esta DA exige determinar a vida útil recalculada de certas peças críticas, substituindo-as se necessário, e também especifica as condições para instalação das peças, conforme especificado em uma DA da Agência Europeia para a Segurança da Aviação (EASA), que é incorporada por referência. A FAA está emitindo esta DA para resolver a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran) (type certificate previously held by Turbomeca, S.A.) Model Makila 1A, Makila 1A1, and Makila 1A2 engines. This AD is prompted by a determination that the accumulated service life of certain critical parts was underestimated. This AD requires determining the recalculated service life of certain critical parts, replacing if necessary, and also specifies conditions for installing the parts, as specified in a European Union 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-2024-1691; Project Identifier MCAI-2023-01269-E; Amendment 39-22847; AD 2024-19-05] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran) (type certificate previously held by Turbomeca, S.A.) Model Makila 1A, Makila 1A1, and Makila 1A2 engines. This AD is prompted by a determination that the accumulated service life of certain critical parts was underestimated. This AD requires determining the recalculated service life of certain critical parts, replacing if necessary, and also specifies conditions for installing the parts, as specified in a European Union 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 November 26, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 26, 2024. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No.FAA-2024-1691; 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 EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email:ADs@easa.europa.eu; website: ad.easa.europa.eu. It is also available at regulations.gov under Docket No. FAA-2024-1691. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available atregulations.gov under Docket No. FAA-2024-1691. FOR FURTHER INFORMATION CONTACT: David Bergeron, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (860) 386-1805; email: David.J.Bergeron@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Safran Model Makila 1A, Makila 1A1, and Makila 1A2 engines. The NPRM published in the Federal Register on June 20, 2024 (89 FR 51858). The NPRM was prompted by EASA AD 2023-0218, dated December 19, 2023 (EASA AD 2023-0218) (also referred to as the MCAI), issued by EASA, which is the Technical Agent for the Member States of the European Un…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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