What was found
CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 - 400, LBL 52, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 143A5400 SHEET 182 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, LBL 52, WL 208.1. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 143A5400 SHEET 182 REV-.