As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(RIGHT WING) TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT. REMOVED AND REPLACED CRACKED ATTACH ANGLE AT TRANSVERSE WEB AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM PER SRM 51-10-02-0G-0 & SRM 51-40-02-0G-