As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DOOR 1R THRESHOLD SUPPORT ANGLE UPPER SURFACE; STA 310-320; RBL 58; CORROSION AROUND 4EA FASTENERS; MRK'D IN RED. / REMOVED COROSION FROM R1 THRESHOLD SUPPORT ANGLE UPPER SURFACE; EVALUATED MATERIAL LOSS: 0.090' LOSSL 0.027' REMAIN: 0.063'. FOUND TO BE OUT OF LIMITS. VERIFIED; LOCATED AND INSTALLED NEW P/N 141A831245 ATAG #5057. APPLIED C.I.C. ON NEW PART. I/A/W SRM 53-10-15-1A-2; SRM: 51-10-02-0G-0; PL #141A8310 DWG #141A8310 REV -.