Resumen
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.
Detalles de la directiva
Número de AD
FAA-2017-0660
Número de documento
2017-27248
Tipo
Rule
Fecha de publicación
December 19, 2017
Fecha de entrada en vigor
January 23, 2018
Fabricante afectado
General Electric Company Turbofan
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2017-0660
Temas
Documentos oficiales
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