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 CRACK AT THE C'' PIT CROSS SLIDE DOOR AFT FR ON FUSELAGE AT FRAME 1260 AND LONGERON 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED ANGLE IAW DC-8 SRM 51-1-3 AND EO NR 00-055 WITH APPROVED 8110-3 DATED 4-13-00.