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- FAA-2025-04782
FAA-2025-04782
Airworthiness Directives; The Boeing Company Airplanes
Resumo Rápido
- Número AD
- FAA-2025-04782
- Autoridade
- FAA
- Data de emissão
- 21/03/2025
- Data efetiva
- 08/04/2025
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
21 de março de 2025
Data Efetiva
08 de abril de 2025
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está corrigindo uma Diretiva de Aeronavegabilidade (DA) que foi publicada no Federal Register. Essa DA se aplica a todos os aviões série Model 737-600, -700, -700C, -800, -900, e -900ER da The Boeing Company. Conforme publicado, as informações de serviço referenciadas em certos parágrafos do texto regulatório estão incorretas, e as datas especificadas nos textos "System Airworthiness Limitation No. 3--Fan Blade Out Conditions" e "System Airworthiness Limitation No. 4--Engine Nacelle Maintenance Errors" da figura 1 do parágrafo (j) do texto regulatório estão incorretas. Este documento corrige esses erros. Em todos os demais aspectos, o documento original permanece inalterado.
The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. As published, the service information referenced in certain paragraphs of the regulatory text is incorrect, and the dates specified in the "System Airworthiness Limitation No. 3--Fan Blade Out Conditions" text and "System Airworthiness Limitation No. 4--Engine Nacelle Maintenance Errors" text of figure 1 to paragraph (j) of the regulatory text are incorrect. This document corrects those errors. In all other respects, the original document remains the same.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 FAA-2023-2234; Project Identifier AD-2023-00963-T; Amendment 39-22960; AD 2025-04-02] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. SUMMARY: The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register . That AD applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. As published, the service information referenced in certain paragraphs of the regulatory text is incorrect, and the dates specified in the “System Airworthiness Limitation No. 3—Fan Blade Out Conditions” text and “System Airworthiness Limitation No. 4—Engine Nacelle Maintenance Errors” text of figure 1 to paragraph (j) of the regulatory text are incorrect. This document corrects those errors. In all other respects, the original document remains the same. DATES: This correction is effective April 8, 2025. The effective date of AD 2025-04-02 remains April 8, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 8, 2025 (90 FR 11109, March 4, 2025). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov by searching for and locating Docket No. FAA-2023-2234; 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 street address for Docket Operations is listed above. Material Incorporated by Reference: • For Boeing material identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; websitemyboeingfleet.com. • 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-2023-2234. FOR FURTHER INFORMATION CONTACT: Luis Cortez-Muniz, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone: 206-231-3958; email: luis.a.cortez-muniz@faa.gov. SUPPLEMENTARY INFORMATION: AD 2025-04-02, Amendment 39-22960 (90 FR 11109, March 4, 2025) (AD 2025-04-02), requires replacing the fasteners on the fan cowl support beam hinge fittings for certain airplanes and, for all airplanes, requires modifying the radial restraint assembly and installing an external doubler at the starter vent, or as an option, installing a serviceable fan cowl. AD 2025-04-02 also requires revising the existing maintenance or inspection program, as applicable, to incorporate new airworthiness limitations. AD 2025-04-02 applies to all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. Need for Correction As published, the service…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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