As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ANGLE RT SIDE WING L/G WHEEL WELL LONGERON BOX STRUCTURE ANGLE STA 1325, RBL 122 AND RBL 124 AREA. REMOVED CORROSION STIFFENER IAW ARM 51-40-02 REV 40. ACCOMPLISHED EI T2018P 53M-4453 REV 0. FABRICATED THE NEW PART. INSTALLED NEW PART IAW SRM 51-40-02 REV 40 AND DWG 65B15093 SHEET 3 REV H. JOB COMPLETED AND CONDITION CK NORMAL.