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- 2026-04165
2026-04165
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- 2026-04165
- Autoridade
- FAA
- Data de emissão
- 03/03/2026
- Data efetiva
- 07/04/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
03 de março de 2026
Data Efetiva
07 de abril de 2026
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA está adotando uma nova diretriz de aeronavegabilidade (AD) para todos os helicópteros Airbus Helicopters Model EC120B. Esta AD foi motivada por um relato de restrições no comando cíclico devido ao posicionamento incorreto da malha de aterramento no receptáculo do comando cíclico do piloto, que limitava o movimento completo do comando cíclico do piloto durante o voo. Esta AD exige uma inspeção única da posição da malha de aterramento no receptáculo do comando cíclico do piloto e, dependendo dos resultados, corrigir o posicionamento da malha de aterramento e instalar uma braçadeira de fixação. A FAA está emitindo esta AD para resolver a condição insegura nestes produtos.
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model EC120B helicopters. This AD was prompted by a report of cyclic flight control restrictions due to the incorrect positioning of the bonding braid on the socket of the pilot cyclic stick, which limited full movement of the pilot cyclic stick during flight. This AD requires a one-time inspection of the position of the bonding braid on the socket of the pilot cyclic stick and, depending on the results, correcting the positioning of the bonding braid and installing a binding clamp. 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-2025-5036; Project Identifier MCAI-2024-00748-R; Amendment 39-23267; AD 2026-04-07] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model EC120B helicopters. This AD was prompted by a report of cyclic flight control restrictions due to the incorrect positioning of the bonding braid on the socket of the pilot cyclic stick, which limited full movement of the pilot cyclic stick during flight. This AD requires a one-time inspection of the position of the bonding braid on the socket of the pilot cyclic stick and, depending on the results, correcting the positioning of the bonding braid and installing a binding clamp. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective April 7, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 7, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-5036; 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; 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, 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-2025-5036. FOR FURTHER INFORMATION CONTACT: Steven Warwick, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (817) 222-5225; email: steven.r.warwick@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 EC120B helicopters. The NPRM was published in the Federal Register on November 28, 2025 (90 FR 54601). The NPRM was prompted by EASA AD 2024-0243, dated December 13, 2024 (EASA AD 2024-0243) (also referred to as the MCAI), issued by EASA, which is the Technical Agent for the Member States of the European Union. The MCAI advises of a report that a pilot experienced seve…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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