As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING, REAR SPAR UPPER CAP AT ABOUT STA XORS 1042 FOUND WITH CORROSION. [SUP 05-14-07] REMOVED AS PER SRM 57-21-01 VOLUME II. MATERIAL REMOVED =0.043" ORIGINAL THICKNESS =0.136", REMAINING THICKNESS =0.093" AND FOUND EXCEEDED LIMITS AS PER 57- 20-00 VOLUME I FIGURE 16. REPAIR CARRIED OUT AS PER FEDEX EA 15710-109869.