As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE SKIN FROM STA 1016 TO STA 1088; RBL 15 TO LBL 15. REMOVED CORROSION. ACCOMPLISHED HFEC SURFACE SCAN IAW B737 NDTM PART 6 51-00-00 PROC 23; 51-00-00 PROC 16; 53-30-00 PROC PROC 3; AND PART 4 51-00-00 PROC 2. NO CRACKS NOTED. REPAIRED IAW EA 21-153-03421 REV A.