As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD FUSELAGE LEFT SIDE TRU DOOR AFT LATCH CUT-OUT APPEARS TO BE CRACKED, CRACK RUNS TO END OF SKIN APPROXIMATELY .250 LONG. C-CHECK RO 10/13/2020. REPLACED SKIN AROUND TRU DOOR, IAW CRJ 200 SRM. REFERENCE CONTINUATION FOR WORK PERFORMED. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE.