EASA Regulations for Cfe Company CFE738

EASA AD US-2024-12-03

Engine - High-Pressure Turbine Stage 1 and Stage 2 Disks - Replacement

The Federal Aviation Administration's Airworthiness Directive 2024-12-03 addresses certain CFE Company Model CFE738-1-1B engines. It mandates the replacement of high-pressure turbine (HPT) stage 1 and stage 2 disks suspected to contain iron inclusions due to manufacturing defects. This directive aims to prevent potential structural failures and uncontained engine debris release.