What was found
CRACK ON SUPPORT ANGLE BTW BS 380 TO BS 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 138, REV -. MEASUREMENT OF THE CRACK IS 1.298
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE BTW BS 380 TO BS 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 143A5400, SHEET 138, REV -. MEASUREMENT OF THE CRACK IS 1.298