As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE VERTICAL STIFFNER AT STA 188 AND RBL 69 Z AXIS -10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PLATE & SHIM FROM 2024-T3 AND INSTALLED PER E.O. NR 99-236 WITH APPROVED 8110-3 DATED 1-18-00.