What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 WL 208.1 AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE 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 LBL 13 WL 208.1 AT PASSENGER CABIN. REPLACED THE SUPPORT ANGLE IAW SRM-51-40-02 AND DWG-143A5400 REV-.