As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) ENGINE SENT FOR REPAIR OF UPPER ENGINE MOUNT BOLT HOLES AND FOD DAMAGE. FOLLOWING OVERHAUL LEVEL CLEAN-UP AND NDT OF COMPRESSOR COMPONENTS, THE 1ST STAGE COMPRESSOR STATOR WAS FOUND TO BE CRACKED AT COMPRESSOR TIE ROD BOLT RECESSES.