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- FAA-2026-05574
FAA-2026-05574
Airworthiness Directives; Airbus Helicopters
Resumo Rápido
- Número AD
- FAA-2026-05574
- Autoridade
- FAA
- Data de emissão
- 23/03/2026
- Data efetiva
- —
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
23 de março de 2026
Data Efetiva
Não informada
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA propõe revogar a Diretiva de Aeronavegabilidade (DA) 2019-09-03 e a DA 2021-05-15, que se aplicam a certos helicópteros Airbus Helicopters Modelo AS332C, AS332C1, AS332L e AS332L1. A DA 2019-09-03 requer uma inspeção única do mecanismo de jettison das portas da cabine. A DA 2021-05-15 requer inspeções repetitivas, modificando o sistema de liberação de cada porta deslizante lateral da cabine ou modificando o projeto do sistema de jettison de cada porta deslizante lateral da cabine. Desde que a FAA emitiu a DA 2021-05-15, o fabricante desenvolveu uma modificação pré-requisito para certos helicópteros, determinou que instruções de modificação aprimoradas eram necessárias para a instalação do sistema de liberação da porta deslizante lateral da cabine e determinou que o prazo de conformidade poderia ser estendido. Esta DA proposta exigiria modificar o sistema de liberação de cada porta deslizante lateral da cabine ou modificar o projeto do sistema de jettison de cada porta deslizante lateral da cabine como ação de encerramento das inspeções repetitivas. A FAA está propondo esta DA para resolver a condição insegura nestes produtos.
The FAA proposes to supersede Airworthiness Directive (AD) 2019-09-03 and AD 2021-05-15, which apply to certain Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. AD 2019-09-03 requires a one-time inspection of the jettisoning mechanism of the cabin doors. AD 2021-05-15 requires repetitive inspections, modifying the release system of each cabin lateral sliding plug door or modifying the design of the jettison system of each cabin lateral sliding plug door. Since the FAA issued AD 2021-05-15, the manufacturer developed a prerequisite modification for certain helicopters, determined improved modification instructions were necessary for installation of the release system of the cabin lateral sliding plug door, and determined the compliance time could be extended. This proposed AD would require modifying the release system of each cabin lateral sliding plug door or modifying the design of the jettison system of each cabin lateral sliding plug door as a terminating action for the repetitive inspections. The FAA is proposing 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-2026-2720; Project Identifier MCAI-2023-00668-R] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 2019-09-03 and AD 2021-05-15, which apply to certain Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters. AD 2019-09-03 requires a one-time inspection of the jettisoning mechanism of the cabin doors. AD 2021-05-15 requires repetitive inspections, modifying the release system of each cabin lateral sliding plug door or modifying the design of the jettison system of each cabin lateral sliding plug door. Since the FAA issued AD 2021-05-15, the manufacturer developed a prerequisite modification for certain helicopters, determined improved modification instructions were necessary for installation of the release system of the cabin lateral sliding plug door, and determined the compliance time could be extended. This proposed AD would require modifying the release system of each cabin lateral sliding plug door or modifying the design of the jettison system of each cabin lateral sliding plug door as a terminating action for the repetitive inspections. The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this NPRM by May 7, 2026. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: (202) 493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-2720; 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 NPRM, the mandatory continuing airworthiness information (MCAI) any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For European Union Aviation Safety Agency (EASA) material identified in this proposed 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 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. FOR FURTHER INFORMA…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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