As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT ENGINE COMPRESSOR STALL. SINGLE STG 8 HPC BLADE FAILED .75 INCH FROM BLADE TIP. FATIGUE FAILURE ORIGINATING FROM SMALL FOD/DOD NICK AT LE. MINOR TIP DMG TO REMAINDER OF STG 8. NO OTHER DMG STG 7,8 & 9 HPC BLADES ARE INSTALLED NEW AT EACH HPC DEBLADE.