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- FAA-2026-11178
FAA-2026-11178
Diretivas de Aeronavegabilidade; Helicópteros Airbus
Resumo Rápido
- Número AD
- FAA-2026-11178
- Autoridade
- FAA
- Data de emissão
- 04/06/2026
- Data efetiva
- 09/07/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
04 de junho de 2026
Data Efetiva
09 de julho 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 Modelo H160-B. Esta DA foi motivada por relatórios de uma bateria de radiofarol pessoal (RFP) completamente descarregada instalada em um sistema de jangada de emergência (SJE), bem como um relato em que as cordas conectando os dois SJE ao RFP não estavam corretamente acopladas. Esta DA exige a realização de um teste funcional do RFP e a inspeção da conexão de corda ao SJE. Dependendo dos resultados do teste funcional, esta DA exige realizar o teste funcional novamente ou substituir as peças afetadas, e dependendo dos resultados da inspeção de corda, acoplar corretamente a alça de pulso do RFP à corda do SJE. Esta DA também proíbe a instalação de um RFP com número de peça específico e a conexão de corda ao SJE, a menos que certos requisitos sejam atendidos. A FAA está emitindo esta DA para abordar a condição insegura destes produtos.
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Model H160-B helicopters. This AD was prompted by reports of a fully discharged personal locator beacon (PLB) battery installed on an emergency life-raft system (ELRS), as well as a report where the ropes connecting the two ELRS to the PLB were not correctly attached. This AD requires performing a functional test of the PLB and inspecting the rope connection to the ELRS. Depending on the results of the functional test, this AD requires performing the functional test again or replacing affected parts, and depending on the results of the rope inspection, correctly attaching the wrist strap of the PLB to the ELRS rope. This AD also prohibits the installation of a certain part- numbered PLB and the rope connection to the ELRS, 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-2026-1337; Project Identifier MCAI-2025-01289-R; Amendment 39-23363; AD 2026-11-02] • 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 H160-B helicopters. This AD was prompted by reports of a fully discharged personal locator beacon (PLB) battery installed on an emergency life-raft system (ELRS), as well as a report where the ropes connecting the two ELRS to the PLB were not correctly attached. This AD requires performing a functional test of the PLB and inspecting the rope connection to the ELRS. Depending on the results of the functional test, this AD requires performing the functional test again or replacing affected parts, and depending on the results of the rope inspection, correctly attaching the wrist strap of the PLB to the ELRS rope. This AD also prohibits the installation of a certain part-numbered PLB and the rope connection to the ELRS, unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective July 9, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 9, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-1337; 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, 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-2026-1337. 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 H160-B helicopters. The NPRM was published in the Federal Register on February 23, 2026 (91 FR 8…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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