As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE PERFORMING BOROSCOPE INSPECTION OF THE SECOND STAGE NR 1 ENG HPT BLADES, FOUND LEADING EDGE DENTED IN AREA B WITH AXIAL CRACK APPROX .223 INCH IN LENGTH ON CONCAVE SIDE & INTERSECTING RADIAL CRACKS ON CONVEX SIDE .564 INCH. REPLACED THE NUMBER 1 ENGINE