What was found
CRACK ON INTERNAL ANGLE, AFT UPPER CORNER AT THE LT AFT EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON INTERNAL ANGLE, AFT UPPER CORNER AT THE LT AFT EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.