As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON INTERNAL DOUBLER STA 360 +3' AT STR 28L / BLENDED CORROSION AT STA 360 + 3' STR 28R INTERNAL DOUBLER; ORIGINAL THICKNESS .050'; REMAINING .044'; LOSS OF .006' FOUND OUT OF LIMITS IAW SRM 53-00-01-1A-5. REMOVED CORRODED DOUBLER AND LOCATED; DRILLED AND INSTALLED NEW DOUBLER IAW SRM 51-40-02-0G-0 AND DWG 143A3230 REV. B APPLIED CIC TO NEW DOUBLER IAW AMM 51-21-91-620-802