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 2ND FROM SPAR HAS UPPER END CRACKED. CUT OUT DAMAGED AREA AND FABRICATED FILLER FROM 2024 T3 .032 PO 900534 DIM 3.75 X 2.5 INCH REPAIR ANGLE FROM 7075 T3 040 PO 900226 DIM 7 X 3.5 INCH IAW B727 SRM 51-40-3 FIG 1 52-20-2 FIG 1. PART TREATED & PRIMED IAW B727 SRM 51-10-2. PART INSTALLED IAW B727 SRM 51-40-3 FIG 1.