As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2, FUSELAGE EXTERIOR STA 1766 L21L-L23L SKIN IS BULGED AND RIVETS PULLING. REMOVED FASTENERS IAW DC8 SRM 51-1-21, CHECKED AREA FOR CORROSION, NONE FOUND AT THIS TIME. LONGERON FITTING FOUND TO BE CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51 -1-24. INSTALLED NEW FITTING AND FASTENERS IN SKIN IAW DC8 SRM 51-1-21.