As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A TWO INCH CRACK IN WING CENTER SECTION VERTICAL STIFFENER AT STA 663.75, RBL 6.15. THE STIFFENER WAS REPAIRED IAW EA 5714-01002. A DIP WAS ISSUED TO ACCOMPLISH A VISUAL INSPECTION OF THE STIFFENER FOR CRACKS EVERY 4500 FLIGHT CYCLES AND TO REPLACE BOTH STIFFENERS IAW EA 5714-01002 OP 02-05 PRIOR TO THE ACCUMULATION OF 15,000 FLIGHT CYCLES FROM REPAIR INSTALLATION.