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- FAA-2026-04919
FAA-2026-04919
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- FAA-2026-04919
- Autoridade
- FAA
- Data de emissão
- 13/03/2026
- Data efetiva
- 17/04/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
13 de março de 2026
Data Efetiva
17 de abril de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova Diretiva de Aeronavegabilidade (DA) para todos os helicópteros Airbus Helicopters modelos AS332C, AS332C1, AS332L, AS332L1 e SA330J. Esta DA foi motivada por relatos de trincas por fadiga encontradas nos braços da aranha de mudança de passo do rotor de cauda (RC) devido a um aumento de carga originário de pilares de rolamento degradados. Esta DA requer intervalos de limite de vida útil reduzidos para o pilar de rolamento afetado e requer a substituição do pilar de rolamento afetado antes de exceder esses intervalos. Esta DA também proíbe a instalação do pilar de rolamento afetado em um helicóptero, a menos que certos requisitos sejam atendidos. A FAA está emitindo esta DA para resolver a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, and SA330J helicopters. This AD was prompted by reports of fatigue cracks found on arms of the tail rotor (TR) pitch change spider due to a load increase originating from degraded bearing stacks. This AD requires reduced life limit intervals for the affected bearing stack and requires replacing the affected bearing stack before exceeding these intervals. This AD also prohibits the installation of the affected bearing stack on a helicopter, unless certain requirements are met. 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-2025-5043; Project Identifier MCAI-2024-00780-R; Amendment 39-23279; AD 2026-05-06] • RIN 2120-AA64 ( printed page 12287) AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, and SA330J helicopters. This AD was prompted by reports of fatigue cracks found on arms of the tail rotor (TR) pitch change spider due to a load increase originating from degraded bearing stacks. This AD requires reduced life limit intervals for the affected bearing stack and requires replacing the affected bearing stack before exceeding these intervals. This AD also prohibits the installation of the affected bearing stack on a helicopter, unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 17, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 17, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-5043; 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 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. You may find this material on the EASA website at ad.easa.europa.eu. • You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Parkway, Room 6N-321, 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-2025-5043. FOR FURTHER INFORMATION CONTACT: Michael Yeshiambel, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4133; email: michael.m.yeshiambel@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Airbus Helicopters Model AS332C, AS332C1, AS332L, AS 332L1, and SA330J helicopters. The NPRM was published in the Federal Register on December 8, 2025 (90 FR 56699). The NPRM was prompted by EASA AD 2024-0250, dated December 20, 2024 (EASA AD 2024-0250) (also referred to as the MCAI), which is the Technical Agent for the Member States of the European Union. The MCAI states that there were reports…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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