As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
COMPRESSOR WAS RECEIVED TO REPAIR FOR DAMAGE TO ROTOR. UPON DISASSEMBLY AND INSP, DISCOVERED THAT A SECTION OF SHROUD BETWEEN THE NR 2 VANES AT THE FWD END OF THE IMPELLER (IDENTIFIED AS DIAMETER I) HAD BROKEN OFF. CAUSE COULD NOT BE DETERMINED. HOURS AND CYCLES COULD NOT BE DETERMINED.