As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN PANEL WAS FOUND WITH A DENT. PERFORMED PERMANENT REPAIR IAW CRJ7/9 SRM 53-61-01-001-004-A02, SRM 53-61-01-101-004-A02 STRUCTURAL IDENTIFICATION, AND ALLOWABLE DAMAGE. DEFECT LOCATION: FS 1051.3-FS 1069.75, STRG. 19R - STRG. 20R