Resumen
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.
Detalles de la directiva
Número de AD
FAA-2026-2280
Número de documento
2026-03794
Tipo
Proposed Rule
Fecha de publicación
February 25, 2026
Cierre de comentarios
April 13, 2026
Fabricante afectado
Airbus SAS
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2026-2280
Temas
Documentos oficiales
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