As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING DISASSEMBLY OF ENGINE TO COMPLY WITH GEARBOX INSPECTION AND HOT SECTION INSPECTION METAL FRAGMENTS WHERE FOUND IN THE COMBUSTOR,. INSPECTION OF THE COMPRESSOR REVEALED 3 BROKEN BLADES ON NR 2 IMPELLER S/N 2-03501-353 CAUSING MAJOR DAMAGE DOWN STREAM. PICTURES MVC-001F TO MVC-010F INCLUDED. 2000-12-07TC: EVENT NOTED,LAST FILE 1987 FROM USA.