As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND THE NR 1 ENGINE THRUST REVERSER PANEL NR 7519DS GOUGED ON FORWARD UPPER CORNER. THE STIFFENER WAS REMOVED AND THE GOUGE WAS BLENDED OUT IAW SRM 53-01. A NEW STIFFENER WAS FABRICATED AND INSTALLED IAW DOUGLAS DRAWING NR 5958762, SRM 51-10-3, AND 51-30-2.