As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING FUEL PANEL LANDING 524BT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND BLENDED AREAS TO BE IN LIMITS IAW SRM 57-20-35-02-05. ORIGINAL THICKNESS .080" REMAINING .075". ALL BLENDED RIVETS MEASURE MORE THAN .179". VERIFIED BLENDS ARE CRACK FREE IAW NTM 51-00-06-910-801 PT 1. APPLIED ALODINE IAW SRM 51-21-10-02-01, PRIMED IAW SRM 51-25-40-02-01. APPLIED SURFACE PROTECTION IAW SRM 57-20-35-02-05.