What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM-51-40-02 AND DWG-143A5400 REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM-51-40-02 AND DWG-143A5400 REV-.