As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN FS 727, S16L - BL 0 FILLET PANEL PERIMETER + FS 770-908, S20L LAP SPLICE REPAIR OF SCRIBE MARKS, TOOLING DAMAGE BELOW THE LAP SPLICE ALONG S20L BETWEEN FS 727 AND FS 908 AND ALONG THE EDGE OF THE FILLET PANEL AFT OF THE WING. REPAIR DOUBLERS WERE INSTALLED ERA 090669-14, REV INITIAL.