As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON RT RING PAN AT STA Y= 889 LWR SIDE (C PAX). DAMAGE AREA WAS CUT OUT PER SRM 56-20-02 REP 1 FIG 202. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE TRIM-OUT PER NDT SPM 06-10-01.001. ANGLE AND WASHER REPAIR WERE FABRICATED PER SRM 56-20-02 REP 1 FIG 202. REPAIR PARTS WERE INSTALLED PER SRM 51-41-02 AND 51-41-05.