Resumen
We are superseding Airworthiness Directive (AD) 2007-06-12 for certain Airbus Model A330-200 and A330-300 airplanes. This new AD reduces the compliance times for reinforcing the structure of the center fuselage. This AD was prompted by a new fatigue and damage tolerance evaluation that revealed the compliance time for an existing reinforcement of the fuselage has to be reduced. We are issuing this AD to prevent fatigue cracking of the fuselage, which could result in reduced structural integrity of the fuselage.
Detalles de la directiva
Número de AD
FAA-2014-0061
Número de documento
2014-19725
Tipo
Rule
Fecha de publicación
September 3, 2014
Fecha de entrada en vigor
October 8, 2014
Fabricante afectado
Airbus
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2014-0061
Temas
Documentos oficiales
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