As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE INSPECTION PHASE, A CRACK IS DETECTED IN A BLADE WITHOUT REPAIR IAW SP1100G-B-72-35-30-00A-310A-B. DO A VISUAL INSPECTION OF THE HIGH PRESSURE COMPRESSOR (HPC) ROTOR ASSEMBLY FOR SERVICEABILITY TABLE 10. HPC 8TH STAGE (IBR) ROTOR - VISUAL INSPECTION PWA REFERENCE: CAS 21138-R9K8P0 NON REPAIRABLE LIFE LIMITED PART TO BE RETIRED BEFORE END OF LIFE