EASA AD US-2025-05-15
Engine - Stage 2 Turbine Aft Cooling Plate - Airworthiness Limitations Section Revision
The Engine - Stage 2 Turbine Aft Cooling Plate - Airworthiness Limitations Section Revision is a regulatory document addressing airworthiness limitations related to the stage 2 turbine aft cooling plate of certain aircraft engines. It provides updated maintenance and inspection requirements to ensure continued safe operation of affected engine components.