What was found
CRACKE SUPPORT ANGLE BETWEEN BS 380 TO 400, RBL 41.5, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20 REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKE SUPPORT ANGLE BETWEEN BS 380 TO 400, RBL 41.5, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20 REV-.