As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK - FITTING, INBD SIDE OF L/H WING T/E INBD MAIN FLAP T/E MID LINK FITTING, WBL 174. PERFORM SRM 57-53-02-2R-1 REV.92 AND EGAT WORK SHEET NO. 50533 STEP 14 TO 15 14.ASSEMBLE THE REPAIR PARTS WITH BMS 5-95 SEALANT BETWEEN MATING SURFACES. REFER TO 767-300F SRM 51-20-05 15.INSTALL THE FASTENERS. INSTALL THE HEX DRIVE BOLTS WET WITH BMS 5-95 SEALANT.