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