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routineRule

AD FAA-2012-0428

Airworthiness Directives; Airbus Airplanes

Resumen

We are adopting a new airworthiness directive (AD) for all Airbus Model A330-243, -243F, -341, -342, and -343 airplanes. This AD was prompted by reports of cracking of air intake cowls on Rolls-Royce Trent engines, worn and detached attachment links, and fractured thermal anti-ice (TAI) piccolo tubes. This AD requires inspecting piccolo tubes, piccolo tube mount links, the aft side of the forward bulkhead, and outer boundary angles (OBA) for cracks, fractures, and broken links, and corrective actions if necessary. We are issuing this AD to prevent degraded structural integrity of the engine nose cowl in case of forward bulkhead damage in conjunction with a broken piccolo tube, and damage to the engine due to operation in icing conditions with reduced TAI performance.

Detalles de la directiva

Número de AD

FAA-2012-0428

Número de documento

2012-26892

Tipo

Rule

Fecha de publicación

November 9, 2012

Fecha de entrada en vigor

December 14, 2012

Fabricante afectado

Airbus

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2012-0428

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de Airbus →

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