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FAA-2026-04967
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- FAA-2026-04967
- 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 substituindo a Diretiva de Aeronavegabilidade (DA) 2020-09-15 que se aplicava a certos helicópteros Airbus Helicopters modelo AS332C, AS332C1, AS332L e AS332L1. A DA 2020-09-15 exigia a remoção das partes removíveis da instalação do guincho duplo ou a remoção do sistema de degelo e permitia, para certos helicópteros, a revisão do Manual de Voo da Aeronave (MVA) para o helicóptero e a instalação de uma placa informativa como método alternativo de conformidade. Desde a emissão da DA 2020-09-15, análise revelou que medições adicionais de níveis de vibração são necessárias. Esta DA mantém todos os requisitos da DA 2020-09-15 e exige que certos helicópteros realizem medições repetitivas de níveis de vibração em voo e, dependendo dos resultados, executem ações corretivas. A FAA está emitindo esta DA para corrigir a condição insegura nesses produtos.
The FAA is superseding Airworthiness Directive (AD) 2020-09-15 which applied to certain Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. AD 2020-09-15 required removing the removable parts of the dual hoist installation or removing the de-icing system and allows, for certain helicopters, revising the rotorcraft flight manual (RFM) for the helicopter and installing a placard as an optional method of compliance. Since the FAA issued AD 2020-09-15, analysis revealed that additional vibration level measurements are necessary. This AD retains all the requirements of AD 2020-09-15 and requires for certain helicopters repetitively measuring vibration levels in-flight, and depending on the results, performing corrective actions. 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-2025-5389; Project Identifier MCAI-2024-00716-R; Amendment 39-23284; AD 2026-05-11] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-09-15 which applied to certain Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. AD 2020-09-15 required removing the removable parts of the dual hoist installation or removing the de-icing system and allows, for certain helicopters, revising the rotorcraft flight manual (RFM) for the helicopter and installing a placard as an optional method of compliance. Since the FAA issued AD 2020-09-15, analysis revealed that additional vibration level measurements are necessary. This AD retains all the requirements of AD 2020-09-15 and requires for certain helicopters repetitively measuring vibration levels in-flight, and depending on the results, performing corrective actions. 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. The Director of the Federal Register approved the incorporation by reference of certain other publications listed in this AD as of May 20, 2020 (85 FR 30589, May 20, 2020). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-5389; 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 Airbus Helicopters material identified in this AD, contact Airbus Helicopters, 2701 North Forum Drive, Grand Prairie, TX 75052; phone: (972) 641-0000 or (800) 232-0323; fax: (972) 641-3775; or atairbus.com/en/products-services/helicopters/hcare-services/airbusworld. • 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-2025-5389. FOR FURTHER INFORMATION CONTACT: Matthew Williams, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (316) 946-4134; email: matthew.t.williams@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2020-09-15, Amendment 39-19911 (85 FR 30589, May 20, 2020), (AD 2020-09-15). AD 2020-09-15 applied to Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters, equipped with a dual hoist installation and de-icing system, …
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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