As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVE ACCES PANEL N/P 284A6813-3 ON INTERNAL FWD E/E: CORROSION WAS FOUND ON S-27L BTW STA.348.2 TO STA.380. STRINGER S-27L BTW STA. 348.2 TO STA. 380 WAS REPAIRED PER B737-800 SRM 53-00-03-2R PROCEDURE 1. REPAIR 1. (LP 1173288)