FAA-2026-15283
Diretivas de Aeronavegabilidade; Helicópteros Airbus
Resumo Rápido
- Número AD
- FAA-2026-15283
- Autoridade
- FAA
- Data de emissão
- 29/07/2026
- Data efetiva
- —
- Criticidade
- routine
- Aeronaves afetadas
- Airbus Helicopters H125/AS350
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
29 de julho de 2026
Data Efetiva
Não informada
Prazo de Cumprimento
Antes do próximo voo
Aeronaves Afetadas
Requisitos de Conformidade
Requisitos de Conformidade
Ação Requerida
Apply alignment markings to main rotor pitch rod upper links, perform repetitive inspections, accomplish corrective actions as needed, or alternatively install new pitch rod lever axis attachment screw as terminating modification.
Prazo de Conformidade
Data Limite
14 de setembro de 2026
Comment deadline for proposed AD; compliance deadline not yet established
Recorrência
repetitive inspections required until modification terminating action is completed
Dados extraídos automaticamente via IA do texto original da DA FAA-2026-15283. 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 propõe rescindir a Diretriz de Aeronavegabilidade (AD) 2022-01-01, que se aplica a todos os helicópteros Airbus Helicopters modelo AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS365N2, AS365N3, EC130B4, EC130T2, SA365C1, SA365C2, SA365N e SA365N1. A AD 2022-01-01 exige a aplicação de marcas de alinhamento e inspeções repetitivas das bielas superiores da articulação do comando cíclico do rotor principal e, dependendo dos achados, a execução das ações corretivas aplicáveis. Desde que a FAA emitiu a AD 2022-01-01, o fabricante projetou um novo parafuso de fixação do eixo da alavanca de comando cíclico e emitiu material de modificação aplicável como opção alternativa. Esta AD proposta manteria todas as ações da AD 2022-01-01 e permitiria a modificação como uma ação terminante para as inspeções repetitivas e ações corretivas. Esta AD proposta também proibiria a instalação de certos parafusos de fixação do eixo da alavanca de comando cíclico afetados, a menos que certos requisitos sejam atendidos. A FAA está propondo esta AD para remediar a condição insegura destes produtos.
The FAA proposes to supersede Airworthiness Directive (AD) 2022-01-01, which applies to all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS 365 N2, AS 365 N3, EC130B4, EC130T2, SA 365 C1, SA 365 C2, SA 365 N, and SA 365 N1 helicopters. AD 2022-01-01 requires the application of alignment markings on, and repetitive inspections of, the main rotor (MR) pitch rod upper links and, depending on findings, the accomplishment of applicable corrective actions. Since the FAA issued AD 2022-01-01, the manufacturer designed a new pitch rod lever axis attachment screw and issued applicable modification material as an alternative option. This proposed AD would retain all the actions of AD 2022-01-01 and would allow the modification as a terminating action to the repetitive inspections and corrective actions. This proposed AD would also prohibit installing a certain affected pitch rod lever axis attachment screws unless certain requirements are met. The FAA is proposing 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-2026-7231; Project Identifier MCAI-2026-00112-R] • RIN 2120-AA64 ( printed page 47794) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 2022-01-01, which applies to all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS 365 N2, AS 365 N3, EC130B4, EC130T2, SA 365 C1, SA 365 C2, SA 365 N, and SA 365 N1 helicopters. AD 2022-01-01 requires the application of alignment markings on, and repetitive inspections of, the main rotor (MR) pitch rod upper links and, depending on findings, the accomplishment of applicable corrective actions. Since the FAA issued AD 2022-01-01, the manufacturer designed a new pitch rod lever axis attachment screw and issued applicable modification material as an alternative option. This proposed AD would retain all the actions of AD 2022-01-01 and would allow the modification as a terminating action to the repetitive inspections and corrective actions. This proposed AD would also prohibit installing a certain affected pitch rod lever axis attachment screws unless certain requirements are met. The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this NPRM by September 14, 2026. 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-2026-7231; 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 NPRM, 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 European Union Aviation Safety Agency (EASA) material identified in this proposed 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 the EASA 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. …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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