What was found
LEADING EDGE ATTACH ANGLE FOR WING TO BODY PANEL 191AR IS CRACKED<[01] REMOVED CRACKED ANGLE IAW SRM 51-40-02-0G-00.;[02] DRILLED NEW ANGLE IAW SRM 51-40-02-0G-00 AND BOEING DRAWING 116A3110.;[03] VERIFIED ACTIONS 1 AND 2;[04] VERIFIED STEPS AND OK TO INSTALL;[05] INSTALLED ANGLE IAW SRM 51-40-02-0G-00 AND BOEING DRAWING 116A3110.;[06] VERIFIED ITEM 5<BR>OK TO CIC;[07] RESTORED CIC IAW MM 51-21-91-620-802.;[08] VERIFIED ITEM 7<BR>AUDIT C/W