As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING T/E FLAP LINKS AND STRUCTURE UPPER SKIN SUPPORT ANGLE CRACKED 1 INCH AT XW 19-00. REMOVED DAMAGED SUPPORT ANGLE PER SRM 51-1-21. STOP DRILLED PER SRM 57-2-0. FABRICATED SUPPORT ANGLE PER SRM 51-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED NEW ANGLE PER SRM 51-1-21.