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AD FAA-2013-0879

Airworthiness Directives; General Electric Company Turbofan Engines

Resumen

We are superseding Airworthiness Directive (AD) 2013-24-17 for General Electric Company (GE) GE90-110B1 and GE90-115B turbofan engines with certain high-pressure compressor (HPC) rotor stage 2-5 spools installed. AD 2013-24-17 required removing these spools from service at times determined by a drawdown plan. This AD retains the same requirements as AD 2013-24-17. This AD also adds additional part number (P/N) HPC spools to the applicability. This AD was prompted by reports of cracking on these additional spools. We are issuing this AD to correct the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2013-0879

Número de documento

2017-06715

Tipo

Rule

Fecha de publicación

April 6, 2017

Fecha de entrada en vigor

April 21, 2017

Fabricante afectado

General Electric Company Turbofan

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2013-0879

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company Turbofan →

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