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AD FAA-2013-0879

Airworthiness Directives; General Electric Company Turbofan Engines

Resumo

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.

Detalhes da diretiva

Número da AD

FAA-2013-0879

Número do documento

2017-06715

Tipo

Rule

Data de publicação

April 6, 2017

Data de vigência

April 21, 2017

Fabricante afetado

General Electric Company Turbofan

Criticidade

routine

Emergência

Não

Docket ID

Docket No. FAA-2013-0879

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

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