As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION IN CENTER SHEAR PANEL BETWEEN FR 87-88 FROM LH BUTT LINE 9.5" TO RH BUTT LINE 9.5". BLENDED OUT CORROSION IN CENTER SHEAR PANEL FRAME 87-88 SRM 51-10-03. NOMINAL .063" LOSS .003" REMAINING. -060" LENGTH 1.54' WIDTH 1.42". FOUND TO BE WITH IN LIMITS SRM 53-23-10/AD/AD03.