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- 2024-11143
2024-11143
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Resumo Rápido
- Número AD
- 2024-11143
- Autoridade
- FAA
- Data de emissão
- 22/05/2024
- Data efetiva
- 06/06/2024
- Criticidade
- routine
- Aeronaves afetadas
- Piper PA-28Piper PA-44
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
22 de maio de 2024
Data Efetiva
06 de junho de 2024
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Resumo da Diretiva
A FAA está adotando uma nova Diretiva de Aeronavegabilidade (AD) para certos aviões Piper Aircraft, Inc. (Piper) modelos PA-28-181, PA-28R-201, PA-34-220T e PA-44-180. Esta AD foi motivada por um relato de um furo de parafuso com dupla furação na fixação do espars traseiro da asa, encontrado durante uma inspeção não programada de um avião devido a uma colisão no solo com um automóvel. Esta AD requer inspeção da fixação do espars traseiro da asa e, se discrepâncias forem encontradas, inspeção da fixação do espars dianteiro da asa, execução de ações corretivas conforme necessário, e relatório à FAA quando ações corretivas forem necessárias. A FAA está emitindo esta AD para aborder a condição insegura desses produtos.
The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Model PA-28-181, PA-28R-201, PA- 34-220T, and PA-44-180 airplanes. This AD was prompted by a report of a double-drilled bolt hole of the rear wing spar attachment fitting found during an unscheduled inspection of an airplane due to a ground collision with an automobile. This AD requires inspecting the rear wing spar attachment fitting and, if discrepancies are found, inspecting the forward wing spar attachment fitting, accomplishing corrective actions as required, and reporting to the FAA when corrective actions are required. 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-2024-1302; Project Identifier AD-2024-00213-A; Amendment 39-22749; AD 2024-10-04] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ( printed page 44915) ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. (Piper) Model PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes. This AD was prompted by a report of a double-drilled bolt hole of the rear wing spar attachment fitting found during an unscheduled inspection of an airplane due to a ground collision with an automobile. This AD requires inspecting the rear wing spar attachment fitting and, if discrepancies are found, inspecting the forward wing spar attachment fitting, accomplishing corrective actions as required, and reporting to the FAA when corrective actions are required. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective June 6, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of June 6, 2024. The FAA must receive comments on this AD by July 8, 2024. 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-2024-1302; 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, contact Piper Aircraft, Inc., 2926 Piper Drive, Vero Beach, FL 32960; phone: (772) 567-4361; email:customerservice@piper.com; website: piper.com. • You may view this service information 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-2024-1302. FOR FURTHER INFORMATION CONTACT: Fred Caplan, Aviation Safety Engineer, FAA, East Certification Branch, FAA, 1701 Columbia Avenue, College Park, GA 30337; phone: (404) 474-5507; email: …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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