As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE WAS FOUND WITH TWO .5 INCH CRACKS EMANATING FROM LIGHTNING STRIKE MARKS OVER THE FS 228 FRAME JUST BELOW THE STRINGER 19L SKIN LAP SPLICE. THE CRACKS WERE ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B727 SRM 53-30-3. THE REPAIR WAS DOCUMENTED PER ER/A 366158-14.