As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING UPPER SURFACE TRAILING EDGE WAS FOUND CORRODED AT XORS 1080 TO 1093. REPAIRED IAW ENGINEERING AUTHORIZATION 1-5730-T0347862, PART 1. THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100. CORROSION REWORKED AREA MEASURE AT RIGHT HAND WING AT XORS 1080 TO XORS 1093 UPPER WING SURFACE TRAILING EDGE ORIGINAL THICKNESS 0.130", MATERIAL REMAINING THICKNESS 0.073", EXEEDED LIMIT AS PER SRM 57-00-01-1A FIGURE 101.