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