As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
** CORROSION ** AT AFT CARGO GILGE FLOOR SUPPORT ANGLES STA 767+5' ;S-26L TO S-27R MKD DOT 60-026 WL-155.5. / REMOVED CORROSION AT AFT CARGO BILGE FLOOR SUPPORT 'TEE STA 767+5; S-26L TO S-27R. ORIGINAL THICKNESS .070'; MINIMUM MAT NOTED .046' MATERIAL LOST .024'; FOUND OUT OF LIMITS AS PER REF B737-700 SRM 53-00-53-1A-1; REMOVED AND REPLACED TEE SUPPORT AS PER REF B737-700 SRM 51-40-02-0G-0 & DWG 146A9401