Resumo
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.
Detalhes da diretiva
Número da AD
FAA-2014-0193
Número do documento
2014-28141
Tipo
Rule
Data de publicação
December 5, 2014
Data de vigência
January 9, 2015
Fabricante afetado
Airbus
Criticidade
routine
Emergência
Não
Docket ID
Docket No. FAA-2014-0193
Tópicos
Documentos oficiais
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