As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMPLISHING FEA 1-5710-F0308148 FOUND POSSIBLE CRACK ON CORNER OF LT WING REFUEL DOOR PNL 519CB. VERIFIED CRACK EXTENDS FROM PANEL EDGE TO THE NEAREST FASTENER HOLE. CUT OUT DAMAGE IAW SRM 57-40-02 REPAIR 7, FIG 202. PERFORMED HFEC INSPECTION IAW NTM CHAPTER 20-00-00 PART 6, NO DEFECTS NOTED. FABRICATED & INSTALLED DOUBLER & FILLER IAW SRM 57-40-02 REPAIR 7 FIG 202. NEED COUNTERSINK & PRIMED.