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AD FAA-2024-1883

Airworthiness Directives; General Electric Company Engines

Resumen

The FAA is adopting a new airworthiness directive (AD) for all General Electric Company (GE) Model CF34-10E2A1, CF34-10E5, CF34- 10E5A1, CF34-10E6, CF34-10E6A1, CF34-10E7, and CF34-10E7-B engines with certain part-numbered high-pressure turbine (HPT) shroud/low pressure turbine (LPT) nozzle assemblies installed. This AD was prompted by a report of failed retention features of the inner and outer support air ducts (commonly referred to as spoolies) discovered during engine disassembly. This AD requires a visual inspection of the combustion case for wear and gouges, repair if necessary, and rework of the affected HPT shroud/LPT nozzle assemblies to add a positive retention of the support air duct. The FAA is issuing this AD to address the unsafe condition on these products.

Detalles de la directiva

Número de AD

FAA-2024-1883

Número de documento

2025-09205

Tipo

Rule

Fecha de publicación

May 22, 2025

Fecha de entrada en vigor

June 26, 2025

Fabricante afectado

General Electric Company

Criticidad

routine

Emergencia

No

Docket ID

Docket No. FAA-2024-1883

Temas

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Documentos oficiales

Ver todas las ADs de General Electric Company →

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