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 ROUNTINE INSP MX FOUND A CRACK ON THE LT HEAVY FRAME ANGLE AT FS 288 FWD BEND RADIUS, 1.4" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-053. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.