As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN BETWEEN FS 1031.00 TO FS1051.00 AND STRINGER 21R TO STGR 26R WAS REPORTED WITH MULTIPLE DAMAGES CONSISTING OF NICKS THAT WERE BLENDED SMOOTH AND GROUPED IN LOCATIONS DENOTED AS DETAILS A THROUGH L. PERFORM PERMANENT REPAIR JAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-001-003-A02, FIGURE 53-61-01-991-806, ITEMS 1.