As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION, CORROSION WAS FOUND AT STRINGER SECTIONS P1 LT AND RT BETWEEN C48 AND C49 STRINGERS. STRINGERS WERE REMOVED FOR REPLACEMENT AND CORROSION WAS FOUND AT CROWN SKIN AND IN A DOME-NUT THRU HOLE AT THE P1 LT INSTALLATION POSITION. REPAIRED IAW EA A2-53R-32445.