As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FORWARD CABIN LT SIDE AT DOOR FRAME 20 UPPER WEB AND ANGLE HAS CORROSION. REMOVED CORROSION FROM PREVIOUS BLENDOUT IAW SRM 51-74-00. AFTER REWORK, BLENDOUT AT WEB L=1.3" W=1.2" REMAINING MATERAL .050" ORIG MATERIAL .071" BLENDED AT ANGLE L=2" W=1" REMAINING MATERIAL .046" ORIG MATERIAL .063". FOUND NO ESTABLISHED DAMAGED LIMITS IAW SRM 53-11-14. R & R WEB AND ANGLE IAW SRM 51-42-11. RETAIN FOR RECORDS.