As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LOWER FUSELAGE SKIN BS 559+80 - 559+112, STRINGER 26L - 26R CORRODED. FOUND OUT OF LIMITS IAW SRM 53-00-31. BLENDED DAMAGE IAW SRM 51-21-06. PERFORMED ULTRASONIC THICKNESS OF SKIN IAW NDTM 51-20-04. FOUND WITHIN LIMITS IAW EA 26-2015-100.