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- 2024-28552
2024-28552
Diretivas de Aeronavegabilidade; Aviões Cirrus Design Corporation
Resumo Rápido
- Número AD
- 2024-28552
- Autoridade
- FAA
- Data de emissão
- 06/12/2024
- Data efetiva
- 23/12/2024
- Criticidade
- routine
- Aeronaves afetadas
- Cirrus SR22Cirrus SR20Robinson R22
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
06 de dezembro de 2024
Data Efetiva
23 de dezembro de 2024
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Resumo da Diretiva
A FAA está adotando uma nova diretiva de aeronavegabilidade (DA) para certos aviões Cirrus Model SR20, SR22 e SR22T, fabricados pela Cirrus Design Corporation (Cirrus). Esta DA foi motivada por um relato de falha da alavanca de potência superior. Esta DA exige inspeções repetitivas (visuais) da alavanca de potência superior para detectar qualquer trinca(s) e, dependendo dos resultados de qualquer inspeção visual, inspecionar (por líquido penetrante fluorescente) ou substituir a alavanca de potência superior. Esta DA também exige a comunicação de todos os resultados de inspeção à FAA. A FAA está emitindo esta DA para corrigir a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR20, SR22, and SR22T airplanes. This AD was prompted by a report of failure of the upper power lever. This AD requires repetitively inspecting (visual) the upper power lever for any crack(s) and depending on the results of any visual inspection, either inspecting (fluorescent penetrant) or replacing the upper power lever. This AD also requires reporting all inspection results to the FAA. 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-2024-2546; Project Identifier AD-2024-00574-A; Amendment 39-22902; AD 2024-24-11] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (Cirrus) Model SR20, SR22, and SR22T airplanes. This AD was prompted by a report of failure of the upper power lever. This AD requires repetitively inspecting (visual) the upper power lever for any crack(s) and depending on the results of any visual inspection, either inspecting (fluorescent penetrant) or replacing the upper power lever. This AD also requires reporting all inspection results to the FAA. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective December 23, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of December 23, 2024. The FAA must receive comments on this AD by January 21, 2025. 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 under Docket No. FAA-2024-2546; 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 Cirrus material identified in this AD, contact Cirrus Design Corporation, 4515 Taylor Circle, Duluth, MN 55811; phone: (218) 788-3000; fax: (218) 788-3525; email:fieldservice@cirrusaircraft.com; website: cirrusaircraft.com. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available atregulations.gov under Docket No. FAA-2024-2546. FOR FURTHER INFORMATION CONTACT: Gregory Koenig, Aviation Safety Engineer, FAA, 1801 S Airport Road, Wichita, KS 67209; phone: (847) 294-7127; email: gregory.l.koenig@faa.gov. SUPPLEMENTARY INFORMATION: Comments …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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