As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF FASTENERS FROM TENSION TIE AT STA 920 RT FOUND 5 HOLES IN FRAME PLUGGED. REMOVED DAMAGE, NDT AREA, REPAIRED TENSION TIE AT BS 920 RT PER B747 SRM 53-10-11 FIG 2 PG 17-35 AND FRAME SECTION FROM STR 6R - 12R PER B747 SRM 53-10-04 FIG 137 PG 897 - 905.