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- 2024-05191
2024-05191
Diretivas de Aeronavegabilidade; Bombardier, Inc., Aeronaves
Resumo Rápido
- Número AD
- 2024-05191
- Autoridade
- FAA
- Data de emissão
- 12/03/2024
- Data efetiva
- 16/04/2024
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
12 de março de 2024
Data Efetiva
16 de abril de 2024
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo a Diretriz de Aeronavegabilidade (AD) 2021-20-13, que se aplicava a determinados aviões Bombardier, Inc., Modelo CL-600-2B16 (Variante 604). A AD 2021-20-13 exigia lubrificação repetitiva e inspeções visuais detalhadas (DVI) repetitivas e inspeções por ensaios não destrutivos (NDT) dos pinos inferiores do cilindro de amortecimento do trem de pouso principal (MLG), e substituição se necessário. Esta AD continua a exigir a lubrificação e as inspeções especificadas na AD 2021-20-13 até que o conjunto do cilindro de amortecimento do MLG seja modificado pela substituição da bucha do braço de arrasto e instalação de novos componentes de articulação dinâmica. Esta AD foi motivada por uma nova solução de projeto para essa possível falha do pino inferior do cilindro de amortecimento. A FAA está emitindo esta AD para corrigir a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2021-20- 13, which applied to certain Bombardier, Inc., Model CL-600-2B16 (604 Variant) airplanes. AD 2021-20-13 required repetitive lubrication and repetitive detailed visual inspections (DVI) and non-destructive test (NDT) inspections of the main landing gear (MLG) shock strut lower pins, and replacement if necessary. This AD continues to require the lubrication and inspections specified in AD 2021-20-13 until the MLG shock strut assembly is modified by replacing the trailing arm bushing and installing new dynamic joint components. This AD was prompted by a new design solution for this potential failure of the shock strut lower pin. 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-2023-2001; Project Identifier MCAI-2023-00666-T; Amendment 39-22676; AD 2024-03-06] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2021-20-13, which applied to certain Bombardier, Inc., Model CL-600-2B16 (604 Variant) airplanes. AD 2021-20-13 required repetitive lubrication and repetitive detailed visual inspections (DVI) and non-destructive test (NDT) inspections of the main landing gear (MLG) shock strut lower pins, and replacement if necessary. This AD continues to require the lubrication and inspections specified in AD 2021-20-13 until the MLG shock strut assembly is modified by replacing the trailing arm bushing and installing new dynamic joint components. This AD was prompted by a new design solution for this potential failure of the shock strut lower pin. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 16, 2024. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of April 16, 2024. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of November 18, 2021 (86 FR 57033, October 14, 2021). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2023-2001; 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 address for Docket Operations is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For service information identified in this final rule, contact Bombardier, ( printed page 17720) Inc., 200 Côte-Vertu Road West, Dorval, Québec H4S 2A3, Canada; North America toll-free telephone 1-866-538-1247 or direct-dial telephone 1-514-855-2999; email ac.yul@aero.bombardier.com; website bombardier.com. • You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th Street, 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-2023-2001. FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2021-20-13, Amendment 39-21751 (86 FR 57033, October 14, 2021) (AD 2021-20-13). AD 2021-20-13 applied to certain Bombardier, Inc., Model CL…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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