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- 2025-03401
2025-03401
Diretivas de Aeronavegabilidade; Aviões da The Boeing Company
Resumo Rápido
- Número AD
- 2025-03401
- Autoridade
- FAA
- Data de emissão
- 04/03/2025
- Data efetiva
- 08/04/2025
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
04 de março de 2025
Data Efetiva
08 de abril de 2025
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (DA) para todos os aviões das séries Boeing Company Modelo 737-600, -700, -700C, -800, -900 e -900ER. Esta DA foi motivada por dois eventos de desprendimento de pá de ventilador do motor (FBO) que resultaram na separação de partes da capota de entrada do motor e da capota de ventilador do avião. Em um evento, partes da capota de ventilador danificaram a fuselagem, causando perda de pressurização e subsequente descida de emergência. Esta DA exige a substituição de fixadores especificados do reforço posterior da capota de entrada para certos aviões; para certos outros aviões, inspeção do fixador do reforço posterior da capota de entrada e substituição dos fixadores se rebites forem encontrados, e, para todos os aviões, substituição dos espaçadores de amortecimento utilizados na fixação da capota de entrada ao envoltório do ventilador do motor; ou, como opção, instalação de uma capota de entrada em condições de serviço. Esta DA também exige a revisão do programa existente de manutenção ou inspeção, conforme aplicável, para incorporar novas limitações de aeronavegabilidade (ALs). A FAA está emitindo esta DA para resolver a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by two engine fan blade-out (FBO) events that resulted in the separation of engine inlet cowl and fan cowl parts from the airplane. In one event, fan cowl parts damaged the fuselage, which caused loss of pressurization and subsequent emergency descent. This AD requires replacing specified inlet cowl aft bulkhead fasteners for certain airplanes; for certain other airplanes, inspecting the inlet cowl aft bulkhead fastener and replacing the fasteners if rivets are found, and, for all airplanes, replacement of the crushable spacers used in the attachment of the inlet cowl to the engine fan case; or as an option, installing a serviceable inlet cowl. This AD also requires revising the existing maintenance or inspection program, as applicable, to incorporate new airworthiness limitations (AWLs). 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-2023-2236; Project Identifier AD-2023-00962-T; Amendment 39-22959; AD 2025-04-01] • RIN 2120-AA64 ( printed page 11103) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by two engine fan blade-out (FBO) events that resulted in the separation of engine inlet cowl and fan cowl parts from the airplane. In one event, fan cowl parts damaged the fuselage, which caused loss of pressurization and subsequent emergency descent. This AD requires replacing specified inlet cowl aft bulkhead fasteners for certain airplanes; for certain other airplanes, inspecting the inlet cowl aft bulkhead fastener and replacing the fasteners if rivets are found, and, for all airplanes, replacement of the crushable spacers used in the attachment of the inlet cowl to the engine fan case; or as an option, installing a serviceable inlet cowl. This AD also requires revising the existing maintenance or inspection program, as applicable, to incorporate new airworthiness limitations (AWLs). The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective 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. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-2236; 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 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-2023-2236. 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: 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 The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. The NPRM published in the Federal Register on December 12, 2023 (88 FR 86084). The NPRM was prompted…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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