As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF THE STRINGER 14L SKIN LAP JOINT PER AD 2003- 08-15, REVEALED A CRACKED FASTENER HOLE AT FS 500A+10 & ANOTHER AT FS 500B+15. THE CRACKS WERE REMOVED WITH SKIN CUTOUTS (1 X 4 & 1 X 7 INCH RESPECTIVELY). THE CUTOUTS WERE REPAIRED WITH ALUMINUM DOUBLERS PER BAC 737 SRM 53-30-3 FIG 42 AND DOCUMENTED PER ER/A 089542-14.