As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REF AMES NR 0460. THE FUSELAGE SKIN IS WORE THROUGH AND CRACKED AT THE FWD LWR EDGE OF THE CUTOUT FOR THE HOR STAB ON THE RIGHT SIDE REPAIRED FUSELAGE SKIN ON THE FWD LOWER EDGE OF CUTOUT FOR HORZ STAB IAW B767 SRM 53-60-01 REPAIR 3. SEE BACK AND PARTIAL WORKSH EETS 1 AND 2 FOR PARTIAL WORK ACCOMPLISHED ADD EMP:V921497