As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C TAIL CONE ACCESS PANEL SUPPORT ANGLE RIGHT DENTED. SUPPORT DENTED AREA SMOOTHED & MEASURED D/Y 0.75"X0.040"=18.75 BEYOND LIMIT SRM 51-80-01VIIR38. SUPPORT ANGLE FAB BOEING DWG AKC7546. HEAT TREAT PER DPS 7.00-1 & HARDNESS VALUE HRB 58.5 PER DPS 1.05-3. HOLES TRANSFERRED SRM 51-35-01VIIR38. NEW SUPPORT TREAT & PAINT SRM 51-21-01VIIR38. INSTL PER SRM 51-35-01VIIR38.