As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 3 PYLON ACCESS PANEL CUT-OUT SKIN FOUND WORN AT PANEL 472AR. REPAIR: THE EFFECTED INNER DOUBLER WAS TRIMMED. THE TRIMMED EDGE WAS NDT INSPECTED. REPAIR SKIN WAS INSTALLED WITH HILOCK FASTENERS TO RESTORE THE TRIMMED OUT AREA. A MODIFIED STEEL WEAR PLATE WAS INSTALLED ON THE SKIN ASSEMBLY SURFACE TO PROVIDE FOR ACCESS DOOR LATCH ENGAGEMENT.