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2022-27007
Airworthiness Directives; BAE Systems (Operations) Limited Airplanes
Resumo Rápido
- Número AD
- 2022-27007
- Autoridade
- FAA
- Data de emissão
- 12/12/2022
- Data efetiva
- 27/12/2022
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
12 de dezembro de 2022
Data Efetiva
27 de dezembro de 2022
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2005-06-14, que se aplicava a certos aviões das séries British Aerospace Model BAe 146 e Model Avro 146-RJ. A DA 2005-06-14 exigia inspeções repetitivas quanto a trincas nos elos externos dos amortecedores laterais do trem de pouso principal (TPP) e ações corretivas, se necessário. A DA 2005-06-14 também fornecia uma ação de término opcional para as inspeções repetitivas. Desde que a FAA emitiu a DA 2005-06-14, foi relatado um caso de trinca adicional em um amortecedor lateral do TPP no qual a ação de término foi executada. Esta DA continua exigindo as ações especificadas na DA 2005-06-14 e exige novas inspeções repetitivas quanto a trincas no elo externo do amortecedor lateral do TPP e substituição, se necessário, conforme especificado em uma DA da Autoridade de Aviação Civil (AAC) do Reino Unido, que é incorporada por referência. Esta DA também proíbe a instalação de peças afetadas sob certas condições. A FAA está emitindo esta DA para resolver a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2005-06- 14, which applied to certain British Aerospace Model BAe 146 and Model Avro 146-RJ series airplanes. AD 2005-06-14 required repetitive inspections for cracking of the outer links on the main landing gear (MLG) side stays, and corrective actions if necessary. AD 2005-06-14 also provided an optional terminating action for the repetitive inspections. Since the FAA issued AD 2005-06-14, there has been a report of additional cracking on a MLG side stay on which the terminating action has been done. This AD continues to require the actions specified in AD 2005-06-14 and requires new repetitive inspections for cracking of the MLG side stay outer link and replacement if necessary as specified in a United Kingdom (U.K.) Civil Aviation Authority (CAA) (U.K. CAA) AD, which is incorporated by reference. This AD also prohibits the installation of affected parts under certain conditions. 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-2022-1574; Project Identifier MCAI-2022-01362-T; Amendment 39-22274; AD 2022-25-18] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2005-06-14, which applied to certain British Aerospace Model BAe 146 and Model Avro 146-RJ series airplanes. AD 2005-06-14 required repetitive inspections for cracking of the outer links on the main landing gear (MLG) side stays, and corrective actions if necessary. AD 2005-06-14 also provided an optional terminating action for the repetitive inspections. Since the FAA issued AD 2005-06-14, there has been a report of additional cracking on a MLG side stay on which the terminating action has been done. This AD continues to require the actions specified in AD 2005-06-14 and requires new repetitive inspections for cracking of the MLG side stay outer link and replacement if necessary as specified in a United Kingdom (U.K.) Civil Aviation Authority (CAA) (U.K. CAA) AD, which is incorporated by reference. This AD also prohibits the installation of affected parts under certain conditions. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective December 27, 2022. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of December 27, 2022. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of May 2, 2005 (70 FR 15574, March 28, 2005; corrected April 14, 2005 (70 FR 19681)). The FAA must receive comments on this AD by January 26, 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 under Docket No. FAA-2022-1574; 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, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For U.K. CAA material incorporated by reference in this AD, contact Civil Aviation Authority, Aviation House, Beehive Ring Road, Crawley, West Sussex RH6 0YR, United Kingdom; telephone +44(0) 330 022 4401; emailcontinued.airworthiness@caa.co.uk; website caa.co.uk. • For BAE Systems…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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