As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE / STRINGER / 18A / FS 920-950 : FATIGUE CRACK REPAIR STRINGER 18A WAS FOUND WITH A 4" TYPICAL FATIGUE CRACK AT FS 950. THE STRINGER WAS CUT AT FS 921 AND THE AFT END REMOVED TO ELIMINATE ALL CRACKS. A NEW SECTION OF STRINGER WAS SPLICED IN PER BAC S/B 727-053-0172 AND ER/A 383648-14.