As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENG (222162) HAS 1 EA HPT TURBINE BLADE WITH BURN THROUGH INTO THE INTERNAL CAVITY ON THE CONCAVE SIDE IN AREAS 'B' AND 'C' WITH AN AREA OF LIFTED MATERIAL IN AREA 'C'. NOT ALLOWED PER AMM 72-00-00 CONFIG 2 PG 698.69. OK TO CONTINUE FOR 5 CYC TO MAX PTC 9428 FOR NR 1 ENG REPLACEMENT. REPLACED NR 1 ENG PER MM.