As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS PUNCTURED AT FS 1197+88 BETWEEN STRINGERS 35L & 36L. THE DAMAGE WAS REMOVED WITH A 12 X 12 INCH CUTOUT CENTERED OVER THE STRINGER 36L SKIN LAP JOINT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND STRUCTURAL FILLER PER B767 SRM 53-00-01-2-212 AND ER/A 379789-14, REV A.