As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAJOR REPAIR. R2 DOOR SILL AFT END CORRODED. BLENDED CORROSION ON AFT END OF DOOR SILL. AFTER BLENDING AFT SECTION MEASURED 0.030 & FWD SECTION MEASURED 0.042. ORIGINAL THICKNESS = 0.070. MAX MATERIAL LOSS ALLOWED =0.017. R & R RT 2 DOOR SILL.