As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING LWR SURFACE OF FRONT SPAR CHORD ANGLE HAS EXFOLIATED CORROSION AFT OF NR 5 L/E SLAT T DUCT. REMOVED CORROSION SPAR CHORD METAL. CORROSION BEYOND LIMITS (ORIG THICK 0.316 AFTER BLEND 0.0220). REPAIR STRAP INSTALLED ON UPPER SURFACE OF FRONT SPAR CHORD LWR ANGLE PER AARD 57-30-00-2 PG 2 AND SRM 57-10-4 PG 1-10.