As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"THE FUSELAGE SKIN, BETWEEN STA. 169-STA.173,STR. 0-STR 1 L WAS FOUND WITH A DENT. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) 53-11-01-001-004-A01. SKIN, TOP PANEL. STRUCTURE IDENTIFICATION. B) CRJ7/9 SRM 53-11-01-101-004-A01 ALLOWABLE DAMAGE REFERS TO SRM 53-00-01-101-001-A01, FUSELAGE SKINS AND PLATING, ALLOWABLE DAMAGE. "