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 manufacturing investigation that found improper application of the fastener retorque process at the center wing box (CWB) and belly fairing (BF) junctions could lead to insufficient clamping. 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-2026-3475
Número de documento
2026-06563
Tipo
Proposed Rule
Fecha de publicación
April 3, 2026
Cierre de comentarios
May 18, 2026
Fabricante afectado
Airbus SAS
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2026-3475
Temas
Documentos oficiales
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