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 4R SKIN LAP SPLICE BETWEEN FS 480 & 680 REVEALED A CRACK INDICATION IN THE LOWER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION OF THE ENTIRE LAP CONFIRMED A SINGLE CRACKED FASTENER HOLE BETWEEN FS 640 & 660. THE DAMAGED SECTION OF LAP JOINT WAS CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 377137-14AD.