As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE AT APPROXIMATELY STA 654 TO STA 720 STR 10R TO 10L HAS EVIDENCE OF MULTIPLE SMOKED RIVETS. UPON REMOVAL OF 130 EA FASTENERS FOUND 2 EA. FASENTER HOLES CRACKED AT CROWN STA 654+22 STR 1L AND STR 1R. REAMED 2 EA CRACKED HOLES TO .214 WITH NDT VERIFICATION NO DEFECTS NOTED. RE-INSTALLED 130 EA FASTNERS, IAW B767 SRM 51-40-0251-40-05.