What was found
INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766 - 1806 LONG 17R IS CRACKED. REMOVED L17R AND END FITTING TO FOM. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED L17R & END FITTING IAW DC8 SRM 51-1-21/51-1-20D.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE: C-2, AFT FUSELAGE EMPENNAGE AREA FS 1766 - 1806 LONG 17R IS CRACKED. REMOVED L17R AND END FITTING TO FOM. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED L17R & END FITTING IAW DC8 SRM 51-1-21/51-1-20D.