As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT C CHECK, LEFT WING LEADING EDGE CAVITY INBD VERTICAL SUPPORT ANGLE FOR NR 2 SLAT ACTUATOR IS CRACKED. REMOVED AND REPLACED VERTICAL SUPPORT ANGLE PER SRM 51-30-2. INSTALLED STAINLESS STEEL DOUBLER ON THE SUPPORT ANGLES PER S/B 57-130, N/R 1356.