As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT HAND; L1 DOOR SILL PLATE; SUPPORT STRUCTURE HAS MULTIPLE AREAS OF CORROSION / BLENDED OUT CORROSION AT L1 DOOR SILL PLATE SUPPORT ANGLE IAW B737 SRM 51-10-02. ORIGINAL THICKNESS 0080'; MATERIAL LOSS 0.020'. THE MATEIRAL REMAINING 0.060'; THE AREA FOUND TO BE OUT OF LIMIT IAW B737-700 SRM 53-80-15-1A-1. LOCATED AND DRILLED NEW ANGLE P/N: 141A842-20 IAW B737-700 SRM 51-40-05 AND DWG: 141A840 REV:-. INSTALLED NEW ANGLE IAW B737-700 SRM 51-40-02 AND DWG 141A8110 REV:- ATAG: WN 0016