What was found
CRACK ANGLE ON STOP FITTING, NR 1 RIGHT AFT OVERWING EXIT DOOR. REPLACED IAW SRM 51-30-05 AND 51-30-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ANGLE ON STOP FITTING, NR 1 RIGHT AFT OVERWING EXIT DOOR. REPLACED IAW SRM 51-30-05 AND 51-30-02.