What was found
CRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 52, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DRAWING 143A5400, SHEET 38, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE BTW BS 380 - 400, LBL 52, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DRAWING 143A5400, SHEET 38, REV A.