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 A PUNCTURE HOLE IN THE OUTER SKIN ON THE FUSELAGE AT STA 220 TO 240 AND L25L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D & EO 00-316 WITH APPROVED 8110-3 DATED12/22/00.