As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
"INITIAL INSPECTION: CRACK ON ANGLE BTW AFT SIDE PANEL AND INNER SKIN NEAR OF ACCESS PANEL 832DR AT PASSENGER DOOR. (L1). " "ANGLE BTW AFT SIDE PANEL AND INNER SKIN NEAR OF ACCESS PANEL 832DR AT PASSENGER DOOR WAS REPLACE PER CRJ-900 S.R.M. 51-42-06-001-001-A01 PAR 6.C. AND CRJ-900 S.R.M. 51-42-13-001-001-A01 PAR 6.C AND CRJ-900 S.R.M. 51-42-22-001-001-A01 PAR. 6.C "