As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A 0.040 CRACK AT THE RT WING EXTERNAL SPLICE FITTING AND A .1875 INCH CRACK AT THE MATING STRUCTURE WING CENTER SECTION UPPER SKIN PANEL. THE SPLICE FITTING WAS REPLACED IAW EA 5710-01199. THE SKIN PANEL WAS REPAIRED IAW ECRA 5710-01769.