As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN IS DENTED AT STA 1002 AND STR 14L 2.5 INCHE ABOVE LAP 6 INCHES FROM CUTOUT 2 INCHES FROM REPAIR. REMOVED SKIN PANEL, FABBED NEW SKIN PANEL AND BONDED DOUBLER TO IT AND INSTALLED REPLACEMENT SKIN PANEL ASSEMBLY IAW B737 400 SRM 51 40 02.