As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT STA 1229 XCW=-70 XCW=-75 CENTER WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-00, REV 48 ORIGINAL MATERIAL THICKNESS=0.177" REMAINING THICKNESS = 0.135" MATERIAL REMOVED =0.042" AND FOUND ACCEPTABLE IAW EA 1-5730-154278. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REV 113.