As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LFEC INSPECTION OF THE STRINGER 26R SKIN LAP SPLICE INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN NEAR FS 486. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL LENGTH CONFIRMED A SINGLE CRACK AT FS 486. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM 53-30-3, FIG 5 AND DOCUMENTED PER ER/A 367069-14AD.