As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 AFT SIDE OF FS 683 WEB LWR CHORD CRACKED BETWEEN LONGERON 30L AND 32L LOCATED BETWEEN WING CENTER SECTION LWR SURFACE AND FUSELAGE LWR LOBE VIEWED THROUGH REMOVED STRESS PNLS. REMOVED 1 CLIP STA 683 L30L AND 2 CLIP L30L & 31L RCD LOCATED AND DRILLED 2 NEW CLIP IAW DC8 SRM 51-1-24, INSTALLED ALL THREE CLIP IAW DC8 SRM 51-1-20D.