Resumen
We are adopting a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 series airplanes. This AD was prompted by a report of a crack found in the fuselage during a fatigue test campaign. This AD requires repetitive rototest inspections for cracking; corrective actions if necessary; and modification of the torsion box, which would terminate the repetitive inspections. We are issuing this AD to prevent cracking in the side box beam flange of the fuselage, which could affect the structural integrity of the airplane.
Detalles de la directiva
Número de AD
FAA-2014-0193
Número de documento
2014-28141
Tipo
Rule
Fecha de publicación
December 5, 2014
Fecha de entrada en vigor
January 9, 2015
Fabricante afectado
Airbus
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2014-0193
Temas
Documentos oficiales
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