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2020-25472
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- 2020-25472
- Autoridade
- FAA
- Data de emissão
- 19/11/2020
- Data efetiva
- 24/12/2020
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
19 de novembro de 2020
Data Efetiva
24 de dezembro de 2020
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está revogando a Diretiva de Aeronavegabilidade (DA) 2018-08-01 para helicópteros Airbus Helicopters modelo EC225LP. A DA 2018-08-01 exigia inspeção dos garfos de fixação da barra de comando (garfo) de certos platôs rotativos de rotor principal (platô). Esta nova DA retém os requisitos de inspeção da DA 2018-08-01, expande a aplicabilidade, estabelece um limite de vida útil e adiciona uma inspeção única dos garfos danificados. Esta DA foi motivada pela identificação de números de série adicionais de platô afetados pela condição insegura e pelo estabelecimento de um limite de vida útil para os platôs. A FAA está emitindo esta DA para abordar a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2018-08-01 for Airbus Helicopters Model EC225LP helicopters. AD 2018-08-01 required inspecting the control rod attachment yokes (yoke) of certain main rotor rotating swashplates (swashplate). This new AD retains the inspection requirements of AD 2018-08-01, expands the applicability, establishes a life limit, and adds a one-time inspection of stripped yokes. This AD was prompted by the identification of additional swashplate serial numbers affected by the unsafe condition and the establishment of a life limit for the swashplates. 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-2020-0513; Product Identifier 2019-SW-037-AD; Amendment 39-21321; AD 2020-23-05] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2018-08-01 for Airbus Helicopters Model EC225LP helicopters. AD 2018-08-01 required inspecting the control rod attachment yokes (yoke) of certain main rotor rotating swashplates (swashplate). This new AD retains the inspection requirements of AD 2018-08-01, expands the applicability, establishes a life limit, and adds a one-time inspection of stripped yokes. This AD was prompted by the identification of additional swashplate serial numbers affected by the unsafe condition and the establishment of a life limit for the swashplates. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective December 24, 2020. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of December 24, 2020. ADDRESSES: For service information identified in this final rule, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; telephone 972-641-0000 or 800-232-0323; fax 972-641-3775; or at https://www.airbus.com/​helicopters/​services/​technical-support.html. You may view the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0513. Examining the AD Docket You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-0513; 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 AD, the European Union Aviation Safety Agency (EASA) AD, any service information that is incorporated by reference, any comments received, and other information. The address for Docket Operations is Document Operations, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Matthew Fuller, AD Program Manager, Operational Safety Branch, Airworthiness Products Section, General Aviation & Rotorcraft Unit, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110; email Matthew.Fuller@faa.gov. SUPPLEMENTARY INFORMATION: Discussion The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2018-08-01, Amendment 39-19254 (83 FR 17617, April 23, 2018) (AD 2018-08-01) and add a new AD. AD 2018-08-01 applied to Airbus Helicopters Model EC225LP helicopters with certain serial-numbered swashplates part number (P/N) 332A31-3074-00 or P/N 332A31-3074-01 installed. The NPRM published in the Federal Register on June 3, 2020 (85 FR 34118). The NPRM proposed to require determining the date of manufacture of the swashplate and establishing a life…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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