Resumen
We are adopting a new airworthiness directive (AD) certain Airbus Model A310-203, -221, and -222 airplanes. This AD was prompted by the manufacturer re-classifying slat extension eccentric bolts as principal structural elements with replacement due at or before their calculated fatigue lives. This AD replaces certain slat extension eccentric bolts with new bolts. We are issuing this AD to prevent fatigue cracking, which could result in the loss of structural integrity of the airplane.
Detalles de la directiva
Número de AD
FAA-2012-0414
Número de documento
2012-18579
Tipo
Rule
Fecha de publicación
August 7, 2012
Fecha de entrada en vigor
September 11, 2012
Fabricante afectado
Airbus
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2012-0414
Temas
Documentos oficiales
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