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- FAA-2025-06420
FAA-2025-06420
Airworthiness Directives; General Electric Company Engines
Resumo Rápido
- Número AD
- FAA-2025-06420
- Autoridade
- FAA
- Data de emissão
- 16/04/2025
- Data efetiva
- 21/05/2025
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
16 de abril de 2025
Data Efetiva
21 de maio de 2025
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está substituindo as Diretivas de Aeronavegabilidade (AD) 2020-20-17 e 2021-15-05 para todos os motores General Electric Company (GE) Modelo GE90-110B1 e GE90-115B. A AD 2020-20-17 proíbe a operação de uma aeronave se certas mensagens de status forem exibidas no sistema de indicação de motor e alerta à tripulação (EICAS) e se certas condições estiverem presentes; e como ação terminativa, exige revisão da Lista Mínima de Equipamentos (MEL) aprovada pela FAA, incorporando as restrições de operação na MEL. A AD 2021-15-05 exige substituição inicial e repetitiva do microprocessador do circuito integrado (MN4) do sistema de controle digital total da potência do motor (FADEC). Desde que a FAA emitiu as AD 2020-20-17 e 2021-15-05, o fabricante desenvolveu uma revisão de software para o controle eletrônico do motor (EEC) FADEC que mitiga ainda mais a condição insegura. Esta AD retém todas as ações das AD 2020-20-17 e 2021-15-05, e também exige a atualização do software EEC FADEC para uma versão de software EEC FADEC elegível para instalação como ação terminativa. A FAA está emitindo esta AD para abordar a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2020-20-17 and AD 2021-15-05 for all General Electric Company (GE) Model GE90- 110B1 and GE90-115B engines. AD 2020-20-17 prohibits dispatch of an airplane if certain status messages are displayed on the engine indicating and crew alerting system (EICAS) and if certain conditions are present; and as terminating action, requires revision of the existing FAA-approved minimum equipment list (MEL) by incorporating the dispatch restrictions into the MEL. AD 2021-15-05 requires initial and repetitive replacement of the full authority digital engine control (FADEC) integrated circuit (MN4) microprocessor. Since the FAA issued AD 2020-20-17 and AD 2021-15-05, the manufacturer has developed a software revision for the electronic engine control (EEC) FADEC that further mitigates the unsafe condition. This AD retains all the actions of AD 2020-20-17 and AD 2021-15-05, and also requires upgrading the EEC FADEC software to an EEC FADEC software version eligible for installation as a terminating action. 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-2024-2417; Project Identifier AD-2024-00336-E; Amendment 39-23012; AD 2025-07-10] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-20-17 and AD 2021-15-05 for all General Electric Company (GE) Model GE90-110B1 and GE90-115B engines. AD 2020-20-17 prohibits dispatch of an airplane if certain status messages are displayed on the engine indicating and crew alerting system (EICAS) and if certain conditions are present; and as terminating action, requires revision of the existing FAA-approved minimum equipment list (MEL) by incorporating the dispatch restrictions into the MEL. AD 2021-15-05 requires initial and repetitive replacement of the full authority digital engine control (FADEC) integrated circuit (MN4) microprocessor. Since the FAA issued AD 2020-20-17 and AD 2021-15-05, the manufacturer has developed a software revision for the electronic engine control (EEC) FADEC that further mitigates the unsafe condition. This AD retains all the actions of AD 2020-20-17 and AD 2021-15-05, and also requires upgrading the EEC FADEC software to an EEC FADEC software version eligible for installation as a terminating action. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective May 21, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of May 21, 2025. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of October 23, 2020 (85 FR 63443, October 8, 2020); and September 13, 2021 (86 FR 43409, August 9, 2021). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-2417; 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 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 GE material identified in this AD, contact GE, 1 Neumann Way, Cincinnati, OH 45215; phone: (513) 552-3272; email:aviation.fleetsupport@ge.com; website: ge.com. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803. 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-2024-2417. FOR FURTHER INFORMATION CONTACT: Alexander Thickstun, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (202) 267-8292; email: alexander.m.thickstun@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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