As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING INBOARD LEADING EDGE STIFFENER, ATTACHED TO LEADING EDGE RIB, HAS DOUBLER CRACKED AT LOWER FASTENER ACCESS THROUGH PANEL 6301, JUST OUTBOARD OF FORWARD BOTTLE BOLT. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW REPAIR PER SRM 51-40-2. (M)