As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, LT WING L/E CAVITY WBL 92 INT FRAME STIFFENER 1ST FWD OF SPAR HAS LOWER END CRACKED THRU FASTENER. CUT OUT DAMAGED AREA AND FABBED FILLER FROM 7075-T6 .040 PO 900226 DIM 5 X 2 X 2 INCH AND DOUBLER FROM 7075-T6 .050 PO 900489 DIM 7 X 2 X 2 INCH IAW 727 SRM 57-20-2 FIG 1 & 51-40-3 FIG 1. PARTS TREATED & PRIMED IAW 727 SRM 51-10-2 AND INSTALLED IAW 727 SRM 51-40-3 FIG 1.