As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003-08-15, REVEALED A TOTAL OF 9 CRACKED FASTENER HOLES AT THREE LOCATIONS IN THE JOINT. THE CRACKS WERE REMOVED WITH CUTOUTS OF 15.5 X 1 INCH AND TWO CUTOUTS OF 7.25 X 1 INCH. THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER BAC 737 SRM 53-30-3, FIG 42 AND DOCUMENTED PER ER/A 089522-14AD.