As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FS 364 FRAME CORRODED BETWEEN LBL 26 AND RBL 26. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURES UT-3 MAX .MATERIAL REMAINING IS .079", ORIGINAL IS .080", MATERIAL REMOVED IS .001". WITHIN ALLOWABLE IAW SRM 53-00-00 & SRM 51-21-06, REF SRM 53-21-15-00, FIG 6. TREATED PRIMED & APPLIED TOP COAT IAW SRM 51-21-06.