As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FWD CORE COWL HINGE NOT PINNED CORRECTLY. NO. 2 ENGINE EXHAUST NOZZLE FAIRINGÏ¿½S ACCESS PANEL WAS FOUND TO BE BENT AND TWISTED. PLACED ON TEMP REPAIR REFERENCE EA25-2019-321 FOR DETAILS. C/W PERMANENT REPAIR. R+R RH ENGINE EXHAUST NOZZLE ASSY IAW CRJ200 AMM 78-11-03-000/400-801. OPS CHECK GOOD. THIS TERMINATES EA 25-2019-321. REQUIRES NO FURTHER INSPECTION.