As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR - DURING ROUTINE SHEDULED MAINTENANCE, A CRACK WAS FOUND ON THE LT HEAVY ANGLE AT FS 288. CRACK IS LOCATED AT THE BEND RADIUS APPROXIMATELY 1.6 IN LENGTH. REPAIRED CRACK IN LT HEAVY DOUBLER AT FS 288 IAW EO 09-1900-53-022. RII INSP COMPLIED IAW EO 09-1900-53-022. MATERIALS UTILIZED ARE LISTED ON THE EO.