What was found
INSPECTION TYPE:C1 AFT FUSELAGE TAIL SECTION AT FS 1766-1780 L17R IS CRACKED. REMOVED L17 RT TO FOM LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONGERON AND END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C1 AFT FUSELAGE TAIL SECTION AT FS 1766-1780 L17R IS CRACKED. REMOVED L17 RT TO FOM LOCATED, DRILLED, DEBURRED AND INSTALLED NEW LONGERON AND END FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.