As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SUPPLEMENTAL INFORMATION: ***CORROSION*** INTERNAL BULKHEAD BS1088 RBL35 WL246 UPPER STIFFENER HAS CORROSION.(M ARKED). / REMOVED DAMAGE ON INTERNAL BULKHEAD BS 1088. RBL 35 W/L 246 UPPER STIFFENER. REPAIRED PER ATS ER 17-05334 REV IR AND SWA EA 1-753-32051 REV IR. (L=.50' X D= .006') ORIGINAL THICKNESS .071'. NO FURTHER ACTION REQUIRED.