As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C FUSELAGE INNER SKIN AT STA 1148-1166 STR 20R CRACKED AND CORRODED OUT OF LIMITS. REMOVE CORROSION FOUND OUT OF LIMITS AS PER SRM 51-10-2, CUT OUT DAMAGED AREA AT STA 1148-1166 STR 20R AND NDT INSPECTION AS PER PART 6 51-00-00 FIGURE 4, NO CRACK FOUND. INSTALLED REPAIR AT FUSELAGE INNER SKIN STA 1148-1166 STR 20R AS PER B727 SRM 53-30-3.