As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING UPPER SKIN SURFACE MID SPAR AT APPROX WS 130 FOUND SURFACE CORROSION. CORROSION REMOVED AS PER SRM 51-10-01 REV 116. ORIG THICKHNESS: 0.354 INCH, MATERIAL REMAINING: 0.350 INCH, MATERIAL REMOVED: 0.004 INCH, WITHIN LIMITS PER SRM 57-30-01 FIGURE 1, REV 116.