What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A5400, SHEET 154, 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 - 400, BL 0, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A5400, SHEET 154, REV-.