What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, 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 LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, DRAWING 143A5400, SHEET 38, REV A.