As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, FOUND HOLE DRILLED IN RADIUS OF FRAME AT CUSP FITTING, RH Y=240. FORMED REPAIR ANGLE FROM 7075-0 MATERIAL AND HEAT TREATED TO T-6 CONDITION IAW DER APPROVED ENGINEERING SKETCH A98-R03. DRILLED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21.