Resumen
We are adopting a new airworthiness directive (AD) for certain CFM International S.A. (CFM) CFM56-5B series turbofan engines. This AD was prompted by a corrected lifing analysis by the engine manufacturer that shows the need to identify an initial and repetitive inspection threshold for certain part number (P/N) turbine rear frames (TRFs). This AD requires initial and repetitive inspections of certain P/N TRFs on the low-pressure turbine (LPT) frame assembly. We are issuing this AD to prevent failure of the TRF on the LPT frame assembly, which could lead to engine separation, damage to the engine, and damage to the airplane.
Detalles de la directiva
Número de AD
FAA-2015-2983
Número de documento
2016-01266
Tipo
Rule
Fecha de publicación
January 26, 2016
Fecha de entrada en vigor
March 1, 2016
Fabricante afectado
CFM International S.A. Turbofan
Criticidad
important
Emergencia
No
Docket ID
Docket No. FAA-2015-2983
Temas
Documentos oficiales
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