As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"THE FUSELAGE SKIN PANEL BETWEEN FS1051.3-FS1069.75, STR 19R-STR 20R WAS FOUND WITH A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-001-004-A02 STRUCTURAL ID. B) CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-61-01-101-004-A02 ALLOWABLE DAMAGE."