As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION FOUND AT PRESSURE FLOOR FS 424-559 LBL 36, STR 17. REMOVED COSSOSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT INSP PROCEDURE UT-3 MIN. MATERIAL REMAINING IS .071" WITHIN ALLOWABLE LIMITS OF REO 601R-53-41-666.