As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING; TRANSVERSE WEB O/B ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT / [01] REMOVED AND REPLACED LEFT WING; TRANSVERSE WEB O/B ATTACH ANGLE AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT P/N 115A6260-1 IAW SRM 51-40-02 AND AIPC 57-42-51--02;[02] VERIFIED CORRECTIVE ACTION #1.