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 I/B AFT FLAP SUPPORT FTG FLANGE FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.625 INCH. LEFT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AND10134-2007 7075T6 AS REPAIR ANGLE REPAIR SIZE 2 X 4 INCHES ORG MATERIAL 7075T73 DIE FORGING, CUTOUT SIZE 0.75 X 1.5 INCH AT BOTH FLANGES.