As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INTERNAL HFEC INSPECTION OF THE LOWER FASTENER ROW OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED 2 CRACKS BETWEEN FS 440 AND 460. THE CRACKS WERE CUT OUT OF THE SKIN LAP AND REPAIRED WITH AN ALUMINUM DOUBLER PER B727 SRM 53-30-3, FIG 5 AND ER/A 367499-14AD.