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AD FAA-2017-0660

Airworthiness Directives; General Electric Company Turbofan Engines

Resumo

We are adopting a new airworthiness directive (AD) for certain General Electric Company (GE) GEnx-1B64/P2, -1B67/P2, -1B70/P2, -1B70/ 75/P2, -1B70C/P2, and -1B74/75/P2 turbofan engines. This AD was prompted by a report of the failure of the high-pressure turbine (HPT) stage 1 blade retainer and subsequent in-flight shutdown of the engine. This AD requires inspection of the HPT stage 1 blade retainer. We are issuing this AD to address the unsafe condition on these products.

Detalhes da diretiva

Número da AD

FAA-2017-0660

Número do documento

2017-27248

Tipo

Rule

Data de publicação

December 19, 2017

Data de vigência

January 23, 2018

Fabricante afetado

General Electric Company Turbofan

Criticidade

important

Emergência

Não

Docket ID

Docket No. FAA-2017-0660

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

Ver todas as ADs de General Electric Company Turbofan →

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