As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE UPPER FUSELAGE SKIN WAS FOUND WITH CRACK INDICATIONS AT THE UPPER ROW OF FASTENERS IN THE STRINGER 26R SKIN LAP SPLICE AT FS 662. ALL CRACK DAMAGE WAS REMOVED WITH A 4.25 X 2.75 CUTOUT. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 14 AND ER/A 369202-14, REV A.