As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, RT WING HAS L/E OF FRONT SPAR VERTICAL STIFFENER. REMOVED DAMAGED STIFFENER IAW B-727 SRM 51-30-2. FABBED NEW FROM BAC 1517-1406 PO 3448268 DIM 32 INCHES AND FILLER (SHIM) FROM 7075-T6 .190 PO 314676 DIM 27.5 X 1.5 INCH IAW B-727 SRM 57-10-2 FIG 3 AND 51-20-1. PARTS TREATED AND PRIMED IAW B-727 SRM 51-10-2 AND INSTALLED IAW B-727 SRM 51-30-2.