As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766-1806 LONG 17L IS CRACKED. REMOVED CRACKED LONG 17L AND END FITTING AND REPLACED WITH NEW LONG 17L AND END FITTING IAW DC8 SRM 51-1-20D & 51-1-21. FABBED AND INSTALLED REPAIR ANGLE AND FILLER IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 5 1-1-8.