As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R1 DOOR CUT OUT AFT LOWER CORNER CORRODED FRAME 20R. ORGINAL MATERIAL THICKNESS IN THIS AREA IS .120 TO .160. REMOVED CORROSION .023 TO .031 IN AREAS & FOUND TO BE IN LIMITS IAW SRM 53-11-12 PARA 4A TABLE 1. NDT INSPECTED AREA IAW NTM 51-10-04PB4 TO VERIFY REMAINING MATERIAL.