What was found
LEFT WING TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP DEFLECTION ROLLER SUPPORT ARM ATTACH POINT. REMOVED AND REPLACED ANGLE IAW SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP DEFLECTION ROLLER SUPPORT ARM ATTACH POINT. REMOVED AND REPLACED ANGLE IAW SRM.