FAA-2026-11560
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- FAA-2026-11560
- Autoridade
- FAA
- Data de emissão
- 09/06/2026
- Data efetiva
- 14/07/2026
- Criticidade
- routine
- Aeronaves afetadas
- Airbus Helicopters H125/AS350
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
09 de junho de 2026
Data Efetiva
14 de julho de 2026
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Requisitos de Conformidade
Requisitos de Conformidade
Ação Requerida
Repetitively inspect main gearbox bevel wheel and magnetic plug for particles and perform corrective actions if applicable.
Prazo de Conformidade
Data Limite
14 de julho de 2026
AD effective date; specific inspection intervals defined in incorporated EASA AD 2023-0044
Recorrência
as specified in EASA AD 2023-0044 incorporated by reference
Dados extraídos automaticamente via IA do texto original da DA FAA-2026-11560. Verifique sempre o documento oficial.
DAs Relacionadas de Outras Autoridades
Esta diretiva trata do mesmo problema identificado nas seguintes DAs:
Resumo da Diretiva
A FAA está substituindo a Diretiva de Aeronavegabilidade (AD) 2025-06-04 para todos os helicópteros Airbus Helicopters modelos AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4 e EC130T2. A AD 2025-06-04 exigia inspeções repetitivas da roda cônica da caixa de engrenagens principal (MGB) e do plug magnético da MGB quanto a partículas e a execução de ações corretivas, se aplicável, e proibia a instalação de uma MGB afetada a menos que certos requisitos fossem atendidos. Desde que a FAA emitiu a AD 2025-06-04, a FAA determinou que a AD 2025-06-04 contém erros nos intervalos de conformidade. Esta AD continua a exigir as ações da AD 2025-06-04 e corrige os intervalos de conformidade. A FAA está emitindo esta AD para resolver a condição insegura nestes produtos.
The FAA is superseding Airworthiness Directive (AD) 2025-06-04 for all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. AD 2025-06-04 required repetitively inspecting the main gearbox (MGB) bevel wheel and the MGB magnetic plug for particles and performing corrective actions if applicable and prohibited installing an affected MGB unless certain requirements were met. Since the FAA issued AD 2025-06-04, the FAA determined that AD 2025-06-04 contains errors in the interval compliance times. This AD continues to require the actions of AD 2025-06-04 and corrects the interval compliance times. 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-2025-5032; Project Identifier AD-2025-01042-R; Amendment 39-23373; AD 2026-12-03] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2025-06-04 for all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. AD 2025-06-04 required repetitively inspecting the main gearbox (MGB) bevel wheel and the MGB magnetic plug ( printed page 34747) for particles and performing corrective actions if applicable and prohibited installing an affected MGB unless certain requirements were met. Since the FAA issued AD 2025-06-04, the FAA determined that AD 2025-06-04 contains errors in the interval compliance times. This AD continues to require the actions of AD 2025-06-04 and corrects the interval compliance times. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective July 14, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of May 9, 2025 (90 FR 14723, April 4, 2025). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-5032; 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, the mandatory continuing airworthiness information (MCAI), 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 European Union Aviation Safety Agency (EASA) material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999 000; email:ADs@easa.europa.eu; website easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 10101 Hillwood Parkway, Fort Worth, TX 76177. 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-2025-5032. FOR FURTHER INFORMATION CONTACT: Luna Yang, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (847) 294-7380; email: luna.y.yang@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2025-06-04, Amendment 39-22992 (90 FR 14723, April 4, 2025), (AD 2025-06-04). AD 2025-06-04 applied to all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1,…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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