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AD FAA-2015-2984

Airworthiness Directives; General Electric Company Turbofan Engines

Resumen

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.

Detalles de la directiva

Número de AD

FAA-2015-2984

Número de documento

2016-04031

Tipo

Rule

Fecha de publicación

February 26, 2016

Fecha de entrada en vigor

April 1, 2016

Fabricante afectado

General Electric Company Turbofan

Criticidad

important

Emergencia

No

Docket ID

Docket No. FAA-2015-2984

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company Turbofan →

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