As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FRAME FLANGE AND WEB FORWARD AND AFT FACE FS 216 BETWEEN STR 25-26L. DERIVETED FRAME FLANGE COMMON TO SKIN AT FS X216, BETWEEN STR 25P TO 26P IAW SRM 51-42-05. CUT FRAME FLANGE AND WEB IAW RD 84-53-8048. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. FIT, DRILLED, PROTECTED AND INSTALLED FABRICATED LOOSE REPAIR ANGLE IAW RD 84-53-8048.