As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENG R/H THRUST REVERSER CORE COWL ON INNER AFT EDGE HAS WEAR STRIP CORRODED. REMOVED DAMAGED PARTS IAW SRM 51-40-02 REV. 86. INSTALLED NEW PARTS IAW SRM 51-40-02 REV. 86 AND IPC 78-32-22 REV. 82. JOB COMPLETED AND CONDITION CHECKS NORMAL.