What was found
CRACK ON INTERNAL ANGLES, FWD & AFT UPPER CORNERS AND FWD LOWER CORNER. AT THE RT AFT EMERGENCY EXIT DOOR. THE ANGLES WERE 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 ANGLES, FWD & AFT UPPER CORNERS AND FWD LOWER CORNER. AT THE RT AFT EMERGENCY EXIT DOOR. THE ANGLES WERE REPLACED IAW DWG 9957735, REV G, SRM 51-41-05-0G, 51-41-02-0G, AND 51-41-01-0G.