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 REVEALED 15 CRACK INDICATIONS IN THE SKIN PANEL BETWEEN FS 540 & 727. THE INSPECTIONS WERE PERFORMED PER AD 2003-08-15. THE ENTIRE LAP JOINT WAS TRIMMED OUT AND REPAIRED PER BAC S/B 737-53A1177. THE REPAIR WAS DOCUMENTED PER ER/A 087962-14AD.