As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C2, EMPENNAGE LT FITTING CRACKED FROM LBL 2-LBL 8 SECOND J BEAM FROM BELLY SKIN. PERFORMED HFEC IAW NDT SPM 06-10-01. FOUND CRACK ON FITTING REMOVED FITTING TO FOM. LOCATED DRILLED DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.