What was found
CRACK SUPPORT ANGLE BS 380 TO 400, LBL 14, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, & DWG 143A5400, SHEET 38, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK SUPPORT ANGLE BS 380 TO 400, LBL 14, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, & DWG 143A5400, SHEET 38, REV A.