As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD PIT RT SIDE WALL ATTACH ANGLE AT FRAME 640 S25R- S26R CORRODED AND GOUGED. REMOVED CORROSION IAW SRM 51-10-02 CHECKED LIMITS OF SIDE WALL ANGLE AT FS 640 S25R-S26R. MATERIAL THICKNESS .050 REMOVED MAT .015 REMANING MAT .035 FOUND TO BE OUT OF LIMITS IAW 53-00-53, FIG 101, DETAIL 5 FABRICATED NEW ANGLE ON TRAVLER TII/ 882795. INSTALLED NEW ANGLE AT FS 640 S25R -S26R IAW SRM 51-40-02.