As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TUL - NR 2 ENGINE S-DUCT INNER SKIN BLISTERED AROUND 2 RIVETS APPROX 2 INCH DIAMETER LOCATED 2 SKIN LAPS PLUS RIVET ROWS UP FROM AFT END BETWEEN 6 AND 7 O'CLOCK POSITION. BLENDED CORROSION PER SRM 51-10-1, INSTALLED DOUBLER PER SRM 54-10-3. (M)