As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF FUSELAGE SKIN BETWEEN STA 590-633 BETWEEN STR14L-19L FOUND STRINGER 16L DENTED AND CRACKED AT STA 610. COMPLIED WITH AT SAA/SAT ON NON ROUTINE 181642 W/O NR 87883560001. FABRICATED STRINGER SEGMENT PER DRAWING NR 143N3110-REV AK.