As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:N/A LEFT WHEEL WELL AFT FLAP ENCLOSURE, WEB ASSY ON AFT PORTION WHERE ACT RETRACTS IS CRACKED IN UPPER RADIUS. LOCATED & DRILLED NEW WEB FABRICATED NEW STIFFENER FOR SPOILER A PULLEY BRACKET ON I/B WEB PANEL, FABRICATED PER DC-8 SRM 51 W 18126. INSTALLED NEW WEB & STIFFENER PER DC8 SRM 51-1-21