As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERIOR LOWER FUSELAGE SKIN CRACKED AND BULGED AT LONGERON 35 RIGHT, FS 102. REMOVED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21. REINSTALLED END FITTING, SHEAR TIES AND DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-20D. REPAIRED SKIN IAW REA D853-50299MR. ALODINED AND PRIMED REPAIR DOUBLER IAW DC-8 SRM 51-1-8.