As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RH HEAVY ANGLE CRACKED IN THE BEND RADIUS AT FS 288, FWD LEADING EDGE OF ANGLE, 2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-047 MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.