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- 2024-17338
2024-17338
Diretivas de Aeronavegabilidade; Aviões da The Boeing Company
Resumo Rápido
- Número AD
- 2024-17338
- Autoridade
- FAA
- Data de emissão
- 06/08/2024
- Data efetiva
- 22/08/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
06 de agosto de 2024
Data Efetiva
22 de agosto de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está corrigindo uma diretiva de aeronavegabilidade (DA) que foi publicada no Registro Federal. Essa DA se aplica a todos os aviões Boeing Company Modelo 757. Conforme publicado, o número da DA referenciado em toda a norma final está incorreto. Este documento corrige esse erro. Em todos os outros 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 757 airplanes. As published, the AD number referenced throughout the final rule is incorrect. This document corrects that error. 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 No. FAA-2023-2395; Project Identifier AD-2023-00767-T; Amendment 39-22773; AD 2024-12-09] • 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 757 airplanes. As published, the AD number referenced throughout the final rule is incorrect. This document corrects that error. In all other respects, the original document remains the same. DATES: This correction is effective August 22, 2024. The effective date of AD 2024-12-09 remains August 22, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of August 22, 2024 (89 FR 58257, July 18, 2024). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-2395; 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 ( printed page 63814) 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-2023-2395. FOR FURTHER INFORMATION CONTACT: Wayne Ha, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 562-627-5238; email wayne.ha@faa.gov. SUPPLEMENTARY INFORMATION: Background AD 2024-12-09, Amendment 39-22773 (89 FR 58257, July 18, 2024), requires an inspection or records check of the wing upper skin at the drag fitting attachment holes for any existing repair; repetitive inspections for loose fasteners, skin cracking, and shim migration at the upper link drag fittings, and for cracking in the diagonal brace and diagonal brace fittings; repetitive inspections for cracking of the fastener holes and loose bolt holes; and applicable on-condition actions for all The Boeing Company Model 757 airplanes. Material Incorporated by Reference Under 1 CFR Part 51 The FAA reviewed Boeing Alert Requirements Bulletin 757-57A0073 RB, Revision 3, dated May 5, 2023. This material specifies procedures for a general visual inspection or records check of the wing upper skin at the drag fi…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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