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 FS 897.70 AND FS 969, STR 13L-STR 18L WAS FOUND WITH DAMAGE DUE TO NICKS AT (31) LOCATIONS. PERFORM PERMANENT REPAIR IAW CRJ7/9 SRM 53-51-01-001-002-A02 STRUCTURAL IDENTICATION. B)CRJ7/9 SRM 53-51-01-101-002-A04 / 53-00-01-101-001, ALLOWABLE DAMAGE.