As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C123, VERTICAL STAB TOP STA ZY284 T/E WEB STIFFENER L-ANGLE HAS CORROSION FWD SIDE OF WEB. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 55-2-0. MAT ID PO 331530 S1646835 PER DC8 DRWG 5611400. FAB STIFFENER IAW DC8 DRWG 5611400. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.