What was found
CRACKED SUPPORT ANGLE AT BOOST PUMP, FRONT SPAR UPPER POSITION LT WING. REPLACED THE ANGLE, THREE SHIMS AND FASTENERS. IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 116A3001, SHEET 12, REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED SUPPORT ANGLE AT BOOST PUMP, FRONT SPAR UPPER POSITION LT WING. REPLACED THE ANGLE, THREE SHIMS AND FASTENERS. IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, AND DWG 116A3001, SHEET 12, REV-.