As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON EXTERNAL FUSELAGE SKIN BS887 STR25R TO STR25L<[01] CORRECTION TO TASK DETAIL SHOULD STATE ' CORROSION ON EXTERNAL FUSELAGE SKIN BS887 STR25R TO STR25L FWD OF BUTT JOINT ';[02] REMOVED CORROSION IN AN AREA OF 7.80' X 0.5 0' REMOVED 0.004' ORIGINAL THICKNESS 0.080' FOUND TO BE IN LIMITS PER SRM 53-00-01-1A-5. REAPPLIED PROTECTIVE FINISH AS SRM 53-00-01-1A-5.