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- 2024-20969
2024-20969
Diretivas de Aeronavegabilidade; Helicópteros Leonardo S.p.a.
Resumo Rápido
- Número AD
- 2024-20969
- Autoridade
- FAA
- Data de emissão
- 16/09/2024
- Data efetiva
- 21/10/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
16 de setembro de 2024
Data Efetiva
21 de outubro de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (AD) para todos os helicópteros Leonardo S.p.a. modelo A109C, A109E, A109K2, A109S e AW109SP. Esta AD foi motivada por relatórios de porcas de travamento soltas do rolamento duplo do rotor de cauda, possivelmente causadas por instalação imprópria. Esta AD exige a desmontagem de certos rolamentos duplos do rotor de cauda e sua remontagem de acordo com procedimentos atualizados. Esta AD também proíbe a instalação de certas carcaças de rolamento duplo do rotor de cauda e conjuntos do controle cíclico de passo. Essas ações estão especificadas em uma AD da Agência de Segurança da Aviação da União Europeia (EASA), que é incorporada por referência. A FAA está emitindo esta AD para resolver a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Leonardo S.p.a. Model A109C, A109E, A109K2, A109S, and AW109SP helicopters. This AD was prompted by reports of loose tail rotor duplex bearing locking nuts, possibly caused by improper installation. This AD requires disassembling certain tail rotor duplex bearings and reassembling them in accordance with updated procedures. This AD also prohibits installing certain tail rotor duplex bearing housings and pitch change slider assemblies. These actions are 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-2023-2238; Project Identifier MCAI-2023-00698-R; Amendment 39-22803; AD 2024-15-11] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Leonardo S.p.a. Model A109C, A109E, A109K2, A109S, and AW109SP helicopters. This AD was prompted by reports of loose tail rotor duplex bearing locking nuts, possibly caused by improper installation. This AD requires disassembling certain tail rotor duplex bearings and reassembling them in accordance with updated procedures. This AD also prohibits installing certain tail rotor duplex bearing housings and pitch change slider assemblies. These actions are 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 October 21, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 21, 2024. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-2238; 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. 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: 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. It is also available atregulations.gov under Docket No. FAA-2023-2238. FOR FURTHER INFORMATION CONTACT: William McCully, Aviation Safety Engineer, FAA, International Validation Branch, FAA, 1600 Stewart Ave. Suite 410, Westbury, NY 11590; phone: (404) 474-5548; email: william.mccully@faa.gov. SUPPLEMENTARY INFORMATION: Background EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2023-0105, dated May 23, 2023 (EASA AD 2023-0105), to correct an unsafe condition on Leonardo S.p.A. Model A109C, A109E, A109K2, A109LUH, A109S, and AW109SP helicopters. The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Leonardo S.p.a. Model A109C, A109E, A109K2, A109S, and AW109SP helicopters. The NPRM published in the Federal Register on December 11, 2023 (…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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