As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF THE FUSELAGE SKIN LAP JOINTS PER AD 2003-08 -15 REVEALED CRACKS IN THE STRINGER 4L SKIN LAP JOINT BETWEEN FS 560 & 590. THE CRACKS WERE REMOVED WITH A 32.5 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND DOCUMENTED PER ER/A 090759-14AD.