FAA

FAA-2025-15688

Airworthiness Directives; Various Airplanes

Autoridade

Federal Aviation Administration (EUA)

Data de Publicação

18 de agosto de 2025

Data Efetiva

22 de setembro de 2025

Prazo de Cumprimento

Antes do próximo voo

Resumo da Diretiva

PT-BRTradução automática

A FAA está adotando uma nova diretiva de aeronavegabilidade (DA) para todas as aeronaves com certos conjuntos de fechos rotativos da Pacific Scientific Company (fechos) instalados. Esta DA foi motivada por um relato de defeito de fabricação nos parafusos utilizados dentro do fecho. Esta DA exige a inspeção dos parafusos do fecho e, dependendo dos resultados, a reidentificação do fecho, a substituição dos parafusos e reidentificação do fecho, ou a substituição do fecho. Esta DA também permite, opcionalmente, proibir o uso do assento até que as ações exigidas por esta DA sejam cumpridas. Esta DA também proíbe a instalação de certos fechos em qualquer aeronave. A FAA está emitindo esta DA para corrigir a condição insegura destes produtos.

ENOriginal (Federal Register)

The FAA is adopting a new airworthiness directive (AD) for all airplanes with certain Pacific Scientific Company rotary buckle assemblies (buckles) installed. This AD was prompted by a report of a manufacturing defect in the screws used inside the buckle. This AD requires inspecting the buckle screws, and depending on the results, reidentifying the buckle, replacing the screws and reidentifying the buckle, or replacing the buckle. This AD also allows optionally prohibiting use of the seat until the actions required by this AD are accomplished. This AD also prohibits installing certain buckles on any airplane. The FAA is issuing this AD to address the unsafe condition on these products.

Documentos e Referências

📄 PDF Original 🌐 Federal Register

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Texto Completo da Diretiva

Expandir 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-2024-0230; Project Identifier AD-2023-01064-A,Q,T; Amendment 39-23107; AD 2025-16-09] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all airplanes with certain Pacific Scientific Company rotary buckle assemblies (buckles) installed. This AD was prompted by a report of a manufacturing defect in the screws used inside the buckle. This AD requires inspecting the buckle screws, and depending on the results, reidentifying the buckle, replacing the screws and reidentifying the buckle, or replacing the buckle. This AD also allows optionally prohibiting use of the seat until the actions required by this AD are accomplished. This AD also prohibits installing certain buckles on any airplane. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective September 22, 2025. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of September 22, 2025. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-0230; 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 Parker Meggitt material identified in this AD, contact Parker Meggitt Services, 1785 Voyager Avenue, Simi Valley, CA 93063; phone: 877-666-0712; email:TechSuppor@meggitt.com; website: Meggitt.com/services_and_support/customer_experience/update-on-buckle-assembly-service-bulletins. • 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 atregulations.gov under Docket No. FAA-2024-0230. FOR FURTHER INFORMATION CONTACT: David Kim, Aviation Safety Engineer, FAA, 3960 Paramount Boulevard, Lakewood, CA 90712; phone: 562-627-5274; email: David.Kim@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 airplanes with a restraint system with a Pacific Scientific Company rotary buckle assembly (buckle) part number (P/N) 1111475 (all dash numbers) or P/N 1111548-01 installed having a date of manufacture (DOM) between January 2012 and September 2012 inclusive, or an unknown DOM. The NPRM was published in the Federal Register on February 29, 2024 (89 FR 14783). The NPRM was prompted by a report of a manufacturing defect in the screws used inside the buckle. In the NPRM, for airplanes with the identified bu…

Fonte: Federal Register (federalregister.gov). Texto original em inglês.