What was found
CRACK ON ANGLE BELOW THE NR 1 BEAM, AFT EDGE. R1 DOOR. THE ANGLE WAS REPLACED IAW DWG 9911579, REV L, SRM 51-41-01, AND 51-41-05.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON ANGLE BELOW THE NR 1 BEAM, AFT EDGE. R1 DOOR. THE ANGLE WAS REPLACED IAW DWG 9911579, REV L, SRM 51-41-01, AND 51-41-05.