As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED PANEL, LT WING L/E NR 1 SLAT OTBD CLOSURE PANEL. REMOVED THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG IAW SRM 57-43-01-2R-3, REFER TO SRM 51-70-07-0G-0 REV. 95.