As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG FOUND CRACKED 1.5 INCH LENGTH AT I/B FLANGE AND 0.9 INCH LENGTH AT O/B FLANGE. LT WING I/B MAIN FLAP TO AFT FLAP HINGE ARM FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 REV 43.