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AD FAA-2015-2984

Airworthiness Directives; General Electric Company Turbofan Engines

Resumo

We are adopting a new airworthiness directive (AD) for all General Electric Company (GE) GEnx-1B54, -1B58, -1B64, -1B67, and -1B70 turbofan engine models. This AD was prompted by reports of two separate, single engine in-flight shutdowns (IFSDs) caused by high-pressure turbine (HPT) rotor stage 1 blade failure. This AD requires inspection and conditional removal of affected HPT rotor stage 1 blades. We are issuing this AD to prevent failure of the HPT rotor stage 1 blades, which could lead to failure of one or more engines, loss of thrust control, and damage to the airplane.

Detalhes da diretiva

Número da AD

FAA-2015-2984

Número do documento

2016-04031

Tipo

Rule

Data de publicação

February 26, 2016

Data de vigência

April 1, 2016

Fabricante afetado

General Electric Company Turbofan

Criticidade

important

Emergência

Não

Docket ID

Docket No. FAA-2015-2984

Tópicos

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiais

Ver todas as ADs de General Electric Company Turbofan →

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