What was found
RIGHT WING; 20' INBOARD OF DEFLECTION CONTROL RIB; ATTACH ANGLE TO PANEL SUPPORT IS CRACKED. A045-003 ; / [01] REMOVED ANGLE IAW SRM 51-40-02.; [02] LOCATED & DRILLED FASTENER HOLES IN NEW ANGLE; 115A2156-18 A TAG # A107454; IAW SRM 51-40-05.; [03] INSTALLED NEW ANGLE IAW SRM 51-40-02.; [04] REMOVED AND REPLACED ANGLE; 20' I/B OF DEFLECTION RIB; FOR RIGHT WING UPPER PANEL SUPPORT IAW SRM 51-40-02 & BOEING DWG. # 115A2156 ID:0007 REV.-; [05] INSPECTION CW STEPS 1-4; [06] AUDIT CW