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, FUSELAGE, CABIN FLOOR PANEL AT STA 700 BL 36 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR FILLER AND ANGLE IAW DC8 SRM 51-1-8 PG 16 AND 20 AND 53-2-0 (FIG 1B). (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).