What was found
DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON EXTERIOR SKIN AT STRINGER 15R, APPROX FS 258. REMOVED CORROSION AND INSTALLED 3 X 5 INCH INSERTION PATCH AND 5 X 8 INCH COVER PATCH.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED CORROSION ON EXTERIOR SKIN AT STRINGER 15R, APPROX FS 258. REMOVED CORROSION AND INSTALLED 3 X 5 INCH INSERTION PATCH AND 5 X 8 INCH COVER PATCH.