What was found
CRACK ON SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 184, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 184, REV-.