As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON UPPER WEB AT BS278 LBL18 8' WL 184.5 BELOW NOSE WHEEL WELL TOP PANEL, ACCESS PANEL 113BW. MARKED / REMOVED CORROSION ON UPPER WEB AT BS 278, LBL 18, ORIGINAL THICKNESS IS .050'; MAX MAT REMOVED 1.5'X1.6'X.011' REMAINING THICKNESS IS .039' WEB FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED UPPER WEB BETWEEN BS268 TO BS 288; 8' BELOW NOSE WHEEL WELL TOP PANEL #113 BW IAW SRM 51-40-02 AND DWG #141A7500 84632U 14AUG20.