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AD FAA-2016-7262

Airworthiness Directives; Airbus Airplanes

Resumo

We are superseding Airworthiness Directive (AD) 98-13-14, for certain Airbus Model A320-211, -212, and -231 airplanes. AD 98-13-14 required repetitive inspections of certain fastener holes of the aft fuselage, and corrective action if necessary. This new AD continues to require the actions in AD 98-13-14, with revised inspection compliance times. This AD was prompted by identification of cracks in the fastener holes of the former junction of the aft fuselage, which occurred during a fatigue test; and a determination that certain compliance times specified in AD 98-13-14 must be reduced. We are issuing this AD to address the unsafe condition on these products.

Detalhes da diretiva

Número da AD

FAA-2016-7262

Número do documento

2017-11290

Tipo

Rule

Data de publicação

June 6, 2017

Data de vigência

July 11, 2017

Fabricante afetado

Airbus

Criticidade

routine

Emergência

Não

Docket ID

Docket No. FAA-2016-7262

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

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AD FAA-2016-7262 — Airworthiness Directives; Airbus Airplanes