Resumo
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A350-941 airplanes. This proposed AD was prompted by a determination that double overcoating sealant was not applied during production on certain fasteners in the center wing box (CWB) and belly faring junction for both left-hand (LH) and right-hand (RH) sides, and certain fasteners are also susceptible to rotation. This proposed AD would require replacing each affected part and applying additional head nut cap protection. The FAA is proposing this AD to address the unsafe condition on these products.
Detalhes da diretiva
Número da AD
FAA-2026-2280
Número do documento
2026-03794
Tipo
Proposed Rule
Data de publicação
February 25, 2026
Encerramento dos comentários
April 13, 2026
Fabricante afetado
Airbus SAS
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2026-2280
Tópicos
Documentos oficiais
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