As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK IN FUSELAGE SKIN EIGHT INCHES FORWARD OF STA 727E AND BELOW STRINGER 22L. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5330-03410. A DIP WAS ISSUED TO INSPECT PER PART 2 WITHIN 60,000 FLIGHT CYCLES FROM REPAIR INSTALLATION AND THEN REINSPECT EVERY 25,000 CYCLES.