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
Documentos oficiales
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