As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 3 ENGINE S/N 451539 10TH STAGE COMPRESSOR BLADE T/E TIP AREA HAS A DING 0.036 INCH WITH 0.020 TEAR ON THE CONVEX SIDE. BLENDED BLADE TIP AND REMOVED THE DAMAGED AREAS AND PERFORMED AN INSPECTION TO ENSURE DEFECTS HAVE BEEN REMOVED IAW MD-10-10 AMM 72-36-00-2.