What was found
CRACK UPPER ANGLE BS 694 AND BL 0. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK UPPER ANGLE BS 694 AND BL 0. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 273A9110, SHEET 6, REV A.