As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 060101. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 5613423. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0.