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- FAA-2025-22217
FAA-2025-22217
Diretivas de Aeronavegabilidade; Airbus Helicopters Deutschland GmbH
Resumo Rápido
- Número AD
- FAA-2025-22217
- Autoridade
- FAA
- Data de emissão
- 08/12/2025
- Data efetiva
- 12/01/2026
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
08 de dezembro de 2025
Data Efetiva
12 de janeiro 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 Deutschland GmbH Modelo MBB-BK 117 C-2 e MBB-BK 117 D-2. Esta AD foi motivada por relatórios de desgaste significativo dos mancais esféricos do conjunto de barra de comando e do conjunto de barra de passo. Esta AD requer a medição do movimento radial de certos mancais esféricos dos conjuntos de barra de comando e conjuntos de barra de passo, comunicação dos resultados e, dependendo dos resultados, execução de ação corretiva. Esta AD também proíbe a instalação de certos conjuntos de barra de comando e conjuntos de barra de passo, a menos que certos requisitos sejam atendidos. A FAA está emitindo esta AD para corrigir a condição insegura nesses produtos.
The FAA is adopting a new airworthiness directive (AD) for all Airbus Helicopters Deutschland GmbH Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters. This AD was prompted by reports of significant wear of the spherical bearings of the control rod assembly and pitch link assembly. This AD requires measuring the radial play of certain spherical bearings of control rod assemblies and pitch link assemblies, reporting the results, and depending on the results, taking corrective action. This AD also prohibits installing certain control rod assemblies and pitch link assemblies 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-2025-0214; Project Identifier MCAI-2024-00391-R; Amendment 39-23099; AD 2025-16-02] • 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 Deutschland GmbH Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters. This AD was prompted by reports of significant wear of the spherical bearings of the control rod assembly and pitch link assembly. This AD requires measuring the radial play of certain spherical bearings of control rod assemblies and pitch link assemblies, reporting the results, and depending on the results, taking corrective action. This AD also prohibits installing certain control rod assemblies and pitch link assemblies unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 12, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 12, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-0214; 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-2025-0214. FOR FURTHER INFORMATION CONTACT: Michael Mueller, Aviation Safety Engineer, FAA, 1600 Stewart Avenue Suite 410, Westbury, NY 11590; phone: (847) 294-7543; email: michael.j.mueller@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 Deutschland GmbH Model MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters. The NPRM was published in the Federal Register on February 26, 2025 (90 FR 10705). The NPRM was prompted by AD 2024-0131, dated July 8, 2024 (EASA AD 2024-0131) (also referred to as the MCAI), issued by EASA, which is the Technical Agent for the Member States of the European…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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