As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE LT WING FRONT SPAR CAP AT RIB 17, 1 INCH IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-120-57-004. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER. MAJOR REPAIR.