As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, SURVEY SEQUENCE NR 326-F1-01 FUSELAGE BETWEEN BS443-461 & S22R-26R EXISTING REPAIR DOES NOT CORRELATE TO A SRM. SURVEY SEQ NR 326-F1-01 FX BTN BS443-461 & STR22R-26R EXISTING REPAIR ADD FASTENERS ARE ADDED AND INSTALLED COMMON TO REPAIR DOUBLER AND REPAIR FILLER IAW RS R53-31-36679, THIS REPAIR IS TIME LIMITED TO 30000 TOTAL FLIGHT CYCLES PENDING A DAMAGE TOLERANCE ANALYSIS (DTA) REF EO B767-5330-37332-A FOR REF.