Resumen
We are adopting a new airworthiness directive (AD) for all CFM International S.A. (CFM) Model CFM56-7B engines. This AD requires initial and repetitive inspections of the concave and convex sides of the fan blade dovetail to detect cracking and replacement of any blades found cracked. This AD was prompted by a recent engine failure due to a fractured fan blade, that resulted in the engine inlet cowl disintegrating and debris penetrating the fuselage, causing a loss of pressurization, and prompting an emergency descent. We are issuing this AD to address the unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2018-0380
Número de documento
2018-09338
Tipo
Rule
Fecha de publicación
May 2, 2018
Fecha de entrada en vigor
May 14, 2018
Fabricante afectado
CFM International S.A. Turbofan
Criticidad
critical
Emergencia
Sí
Docket ID
Docket No. FAA-2018-0380
Temas
Documentos oficiales
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