As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ONE CRACK EMINATING FROM RIVET HOLE IN SKIN PANEL APPROXIMATELY 0.125 INCH IN LENGTH AT BS 258 BETWEEN S-19L AND S-20L. REPLACED SKIN PANEL FROM BS223 TO BS259.5 S-19L TO S-24L PER BOEING MESSAGE CGG-ADS-03-00005H. FAA FORM 8110-3 ISSUED.