As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGE FOUND ON FUSELAGE BETWEEN FRAMES 1175 AND 1197 LEFT AT STR 20L. REMOVED DAMAGE PER B767 SRM 53-00-01-2R-29 FIG 201. RII PERFORMED HFEC SURFACE SCAN OF CUT OUT AREA PER B767 NDT 51-00-19 NO FAULTS NOTED. C/W INSTRUCTIONS OF ERA 628660- 14 REV ORG SECTION I REPETITIVE INSP TO BE ACCOMPLISHED PER LOG 1661151. RII INSP OF REPAIR C/W IAW ERA 628660-14 REV ORG. (1161345)