As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND CORRODED ALONG THE S-26L LAP JOINT AT STA 700. REMOVAL OF THE CORROSION RESULTED IN A 3 INCH WIDE BY 10 INCH LONG CUT OUT IN THE OVERLAPPING SKIN ONLY. A PREVIOUS REPAIR DOUBLER IS LOCATED WITHIN 2 INCHES OF THIS REPAIR. IN ACCORDANCE WITH B727 SRM 53-30-3 FIG 14, THE SKIN WAS REPAIRED.