As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN CORRODED AROUND DRAIN PLUG AREA STA 727J S26R TO S27R. FUSELAGE SKIN AT STA 727J S26R - S27R CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. HFEC NIL CRACK FOUND, AND REPAIRED AS PER ECRA 5330-04173 REV- ATTACH MAINT WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 2 ACCOMPLISHED.