EASA AD US-2025-04-13
Engine - High-Pressure Compressor (HPC) 7th-Stage Axial Rotor - Inspections / Replacement
The document titled 'Engine - High-Pressure Compressor (HPC) 7th-Stage Axial Rotor - Inspections / Replacement' is a regulatory directive concerning the inspection and replacement requirements for the 7th-stage axial rotor of the high-pressure compressor in certain aircraft engines. It addresses maintenance procedures to ensure the continued airworthiness and safety of affected engines. Specific aircraft types or engine models are not clearly identified in the provided text.