What was found
DURING SCHDULED ROUTINE STRUCTURAL INSPECTION, DISCOVERED SMALL AREA OF CORROSION APPROX .25 INCH DIAMETER FS 258 AT STRINGER 13L. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED 4.75 X 6.25 INCH COVER PATCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHDULED ROUTINE STRUCTURAL INSPECTION, DISCOVERED SMALL AREA OF CORROSION APPROX .25 INCH DIAMETER FS 258 AT STRINGER 13L. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED 4.75 X 6.25 INCH COVER PATCH.