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- Diretivas de Aeronavegabilidade
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- 2024-23116
2024-23116
Diretivas de Aeronavegabilidade; Aeronaves The Boeing Company
Resumo Rápido
- Número AD
- 2024-23116
- Autoridade
- FAA
- Data de emissão
- 08/10/2024
- Data efetiva
- 12/11/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
08 de outubro de 2024
Data Efetiva
12 de novembro de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretriz de Aeronavegabilidade (DA) 2009-01-02, que se aplicava a certos aviões da série Boeing Model 737-600, -700, -700C, -800 e -900. A DA 2009-01-02 exigia uma inspeção dos longarinas entre a estação de fuselagem (EF) 360 e EF 907 para determinar se certos suportes das extrusões de saída do sistema de ar condicionado (A/C) estavam instalados, inspeções de trincas nos longarinas ao redor dos furos de fixação dos referidos suportes, e reparo se necessário. A DA 2009-01-02 também exigia a instalação de novos conectores melhorados para todos os suportes das extrusões de saída do A/C entre as EF 360 e EF 907. Esta DA foi motivada por numerosos relatos de múltiplas trincas no longarina ao redor dos furos de fixação do suporte da extrusão de saída do A/C, e pela determinação de que certos reparos poderiam desenvolver trincas de fadiga que poderiam resultar na incapacidade do longarina de suportar a carga limite e, portanto, devem ser inspecionados. Esta DA continuaria a exigir as ações especificadas na DA 2009-01-02 e também exigiria inspeções repetitivas de trincas em certos reparos, e reparo se necessário. A FAA está emitindo esta DA para abordar a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2009-01- 02, which applied to certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. AD 2009-01-02 required an inspection of frames between body station (BS) 360 and BS 907 to determine if certain support brackets of the air conditioning (A/C) outlet extrusions are installed, inspections for cracking of the frames around the attachment holes of the subject brackets, and repair if necessary. AD 2009-01-02 also requires installing new, improved fittings for all support brackets of the A/C outlet extrusions between BS 360 and BS 907. This AD was prompted by numerous reports of multiple cracks in the frame around the attachment holes of the support bracket of the A/C outlet extrusion, and the determination that certain repairs might develop fatigue cracks that could result in the inability of the frame to sustain limit load and therefore must be inspected. This AD would continue to require the actions specified in AD 2009-01-02 and would also require repetitive inspections for cracking of certain repairs, and repair if necessary. 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-2023-1886; Project Identifier AD-2023-00429-T; Amendment 39-22841; AD 2024-18-07] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2009-01-02, which applied to certain Boeing Model 737-600, -700, -700C, -800, and -900 series airplanes. AD 2009-01-02 required an inspection of frames between body station (BS) 360 and BS 907 to determine if certain support brackets of the air conditioning (A/C) outlet extrusions are installed, inspections for cracking of the frames around the attachment holes of the subject brackets, and repair if necessary. AD 2009-01-02 also requires installing new, improved fittings for all support brackets of the A/C outlet extrusions between BS 360 and BS 907. This AD was prompted by numerous reports of multiple cracks in the frame around the attachment holes of the support bracket of the A/C outlet extrusion, and the determination that certain repairs might develop fatigue cracks that could result in the inability of the frame to sustain limit load and therefore must be inspected. This AD would continue to require the actions specified in AD 2009-01-02 and would also require repetitive inspections for cracking of certain repairs, and repair if necessary. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 12, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 12, 2024. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of February 27, 2009 (74 FR 4117, January 23, 2009). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-1886; 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-2023-1886. FOR FURTHER INFORMATION CONTACT: Owen F. Bley-Male, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: 206-231-3992; email: Owen.F.Bley-Male@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2009-01-…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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