As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE FIRST 600 HOUR ENG INSPECTION, PERFORMED AXIAL COMPRESSOR BLADE INSPECTION CHECK FOR DAMAGE & SERVICEABILITY, DISCOVERED ONE BLADE HAD FOD DAMAGE AT THE TIP THAT EXCEEDED THE REPAIR LIMITS FOR LEVEL 2 TECHNICIANS. FURTHER DAMAGE TO THE ENG IS UNKNOWN AT THIS TIME DUE TO WAITING ON TOOLING TO COMPLETE FURTHER ANALYSIS OF THE INTERNAL PORTION OF THE ENG. INSPECTED ENG COWLING & FDC AERO FILTER FOR DEBRIS & DAMAGE THAT COULD HAVE RESULTED IN FOD DAMAGE TO ENG BUT DID NOT FIND ANY DISCREPANCIES OR ANOMALIES.