EASA 2024-0040-E

Requires detailed visual inspection for cracks on the engine centrifugal compressor case mount pad weld area and any necessary corrective action(s). AD also provides requirements for reporting and for installation of affected parts. Prompted by a report that a crack was found on an engine’s centrifugal compressor case mount pad weld area, leading to unscheduled engine removal. Further investigation identified non-conforming welding in the location of the failure (lack of welding penetration).