As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, FOUND CRACK RIGHT WING UPPER SKIN PANEL JUST FWD OF NR 10 SPOILER. STOP DRILL AT CRACK RT UPPER SKIN PANEL JUST FWD OF NR 10 SPOILER AS PER SRM 51-10-1. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2 7075-T6 .032 6 INCH BY 2.5 INCH LOT 133261 PO 9318067 AT R/W UPPER SKIN PANEL FWD OF NR 10 SPOILER.