As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE INBD THRUST REVERSER DAMAGED. DAMAGE IS LOCATED NEAR THE CORE COWL VENT PANEL UPPER-FWD CORNER AREA. DAMAGE IS APPROXIMATELY 3 INCHES BY 3 INCHES. DETERMINED BOTH INNER AND OUTER FACE SHEETS ARE DAMAGED AT EDGE OF GRILL CUTOUT.