As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CPCP CHECK INSPECTION, FOUND CRACK APPROXIMATELY 4 INCHES ON FUSELAGE FITTING STA 834 LEFT HAND BETWEEN LONGERON 24 THROUGH LONGERON 21. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-0 AND 51-1-20D. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE TASK CARD NUMBER 93624.