As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BLENDED CORROSION ON WING CENTER SECTION SUPPORT BEAM WEB RT B STA 570, RBL 40.875 IAW SRM 51-10-02 REV 114. REMAINING MATERIAL THICKNESS 0.021". DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 57-10-13 FIG 101 DETAIL III REV 114. REPAIRED DAMAGE IAW DWG NR 27905.1 -057-005-001 REV A.