Resumen
The FAA proposes to adopt a new airworthiness directive (AD) for certain General Electric Company (GE) Model CF34-8C1, CF34-8C5, CF34-8C5A1, CF34-8C5A2, CF34-8C5B1, CF34-8E2, CF34-8E2A1, CF34-8E5, CF34-8E5A1, CF34-8E5A2, CF34-8E5A2HA, CF34-8E6, and CF34-8E6A1 engines. This proposed AD was prompted by reports of in-flight "Engine Degraded" messages from the engine indicating and crew alerting system (EICAS) due to corrosion of the variable geometry (VG) system actuator. This proposed AD would require removing certain electronic engine control (EEC) full authority digital electronic control (FADEC) software versions from service and installing an updated EEC FADEC software that is eligible for installation. The FAA is proposing this AD to address the unsafe condition on these products.
Detalles de la directiva
Número de AD
FAA-2025-3998
Número de documento
2025-20089
Tipo
Proposed Rule
Fecha de publicación
November 18, 2025
Cierre de comentarios
January 2, 2026
Fabricante afectado
General Electric Company
Criticidad
routine
Emergencia
No
Docket ID
Docket No. FAA-2025-3998
Temas
Documentos oficiales
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