As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FRAME AT FS 319 AND FROM STRINGERS 26L TO 26R. REMOVED CORROSION ON FRAME IAW SRM 53-21-06-101-002-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042"7, ORIGINAL IS .050" MATERIAL REMOVED IS .008". CORROSION ON FRAME IS OUT OF LIMITS IAW SRM 53-21-06-101-003-A01 IAW NOTE 1. REPAIRED IAW REO 670-53-21-870 RC161761.