As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SEC 48 UPPER FUSELAGE BETWEEN BS 1896 AND BS 1918 HAS A CUSTER OF 04 DENTS (TWO ARE LOCATED AROUND THE AREA, AND TWO ARE LOCATED OVER A PREVIOUS REPAIR) APPLIED PERMANT REPAIR AT SEC 48 UPPER FUSELAGE LH BTW STA 1896 TO 1918 IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER REPAIR IS SATISFACTORY IAW B757 SRM 51-10-06- 2R