As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE LOWER FUSELAGE SKIN PANEL (P/N: MM690-35146-005)WAS DISCOVERED WITH (2) ELONGATED HOLES NEAR FS1088.20 BETWEEN STGR21 R-STGR22R. PERFORM PERMANENT REPAIR IAW CRJ7/9 STRUCTURAL REPAIR MANUAL (SRM) A) BOMBARDIER REPAIR ENGINEERING ORDER (REO) 690-53-61-877 (REV. -A DATED 2020-07-13). B) 53-61-01-001-003-A02, ITEMS 1 AND C.