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- 2023-10526
2023-10526
Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes
Resumo Rápido
- Número AD
- 2023-10526
- Autoridade
- FAA
- Data de emissão
- 16/05/2023
- Data efetiva
- 31/05/2023
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
16 de maio de 2023
Data Efetiva
31 de maio de 2023
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2019-18-09, que se aplicava a todos os aviões Lockheed Martin Corporation/Lockheed Martin Aeronautics Company modelo 382, 382B, 382E, 382F e 382G; e aviões modelo C-130A, HP-C-130A, EC-130Q, C-130B e C-130H. A DA 2019-18-09 exigia inspeção visual dos acessórios arco-íris superiores e inferiores da asa central quanto a trincas, inspeção por correntes parasitas dos acessórios arco-íris inferiores da asa central quanto a trincas e substituição se necessário. Esta DA foi motivada por uma análise de trincas relatadas que demonstrou que inspeções repetitivas são necessárias para adequadamente abordar trincas nos espigões internos dos acessórios arco-íris inferiores da asa central. Esta DA exige inspeções repetitivas dos acessórios arco-íris superiores e inferiores da asa central quanto a trincas e substituição se necessário. A FAA está emitindo esta DA para abordar a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2019-18- 09, which applied to all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G airplanes; and Model C-130A, HP-C-130A, EC-130Q, C-130B, and C-130H airplanes. AD 2019-18-09 required a visual inspection of the center wing upper and lower rainbow fittings for cracks, an eddy current inspection of the center wing lower rainbow fittings for cracks, and replacement if necessary. This AD was prompted by an analysis of reported cracks showing repetitive inspections are needed to adequately address cracked inner tangs of the center wing lower rainbow fittings. This AD requires repetitive inspections of the center wing upper and lower rainbow fittings for cracks and replacement 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-2023-1044; Project Identifier AD-2023-00593-T; Amendment 39-22436; AD 2023-09-13] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2019-18-09, which applied to all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G airplanes; and Model C-130A, HP-C-130A, EC-130Q, C-130B, and C-130H airplanes. AD 2019-18-09 required a visual inspection of the center wing upper and lower rainbow fittings for cracks, an eddy current inspection of the center wing ( printed page 31160) lower rainbow fittings for cracks, and replacement if necessary. This AD was prompted by an analysis of reported cracks showing repetitive inspections are needed to adequately address cracked inner tangs of the center wing lower rainbow fittings. This AD requires repetitive inspections of the center wing upper and lower rainbow fittings for cracks and replacement if necessary. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective May 31, 2023. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of May 31, 2023. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of October 11, 2019 (84 FR 50730, September 26, 2019). The FAA must receive comments on this AD by June 30, 2023. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: 202-493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov by searching for and locating Docket No. FAA-2023-1044; 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 service information identified in this final rule, contact Lockheed Martin Corporation/Lockheed Martin Aeronautics Company, Airworthiness Office, Dept. 6A0M, Zone 0252, Column P-58, 86 S Cobb Drive, Marietta, GA 30063; telephone 770-494-5444; fax 770-494-5445; emailams.portal@lmco.com. • You may view this referenced service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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