As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING DETAILED INSPECTION OF THE PRESSURE FLOOR SKIN IAW NDT MANUAL, PART 9, 53-41-149. FOUND LT SIDE ATTACHMENT FLANGE AT FS 484 CRACKED ALSO CONFIRMED WITH EDDY CURRENT IAW NDTM 51-20-06. / PART 1. R & R LT ANGLE FLANGE IAW REO 601R-53-41-059, REV B. RESTORED FININSH IAW SRM 51-21-16.