As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED INSPECTION, THE LEFT CANTED RIB CAP P/N 5722206-1 WAS FOUND CRACKED APPROXIMATELY 1 INCH AFT OF THE FORWARD WING SPAR. WHILE REPAIRING THIS CRACK THE UPPER WING TO FUSELAGE CLOSEOUT ANGLE P/N 5720001-3 WAS FOUND CRACKED. THESE CLOSEOUT ANGLES CANNOT BE SEEN UNLESS THE WING TO FUSELAGE FAIRINGS ARE REMOVED AND THUS ARE NEVER INSPECTED DURING NORMAL MAINTENANCE.