As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW SRM 51-40-02-0G AND SRM 51-10-02-0G ITEM 9; DWG 114A5010 SHEET 14 REV C. MEASURE OF CRACK IS: L= 2.019.