Resumen
The FAA is adopting a new airworthiness directive (AD) for certain CFM International, S.A. (CFM) Model LEAP-1A and LEAP-1C engines. This AD was prompted by an investigation of an in-flight shut down event that revealed the aft arm of the high-pressure turbine (HPT) rotor interstage seal had failed. This AD requires removal from service and replacement of the HPT rotor interstage seal for LEAP-1A engines. Since the HPT rotor interstage seal part number is interchangeable between LEAP-1A and LEAP-1C engines, this AD also prohibits installation of these affected parts onto any LEAP-1A or LEAP-1C engine. The FAA is issuing this AD to address the unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2024-2325
Número de documento
2025-02204
Tipo
Rule
Fecha de publicación
February 4, 2025
Fecha de entrada en vigor
March 11, 2025
Fabricante afectado
CFM International, S.A.
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2024-2325
Temas
Documentos oficiales
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