What was found
A -204 DOT 01; LH WING L/E ATTACH ANGLE CRACKED AT FASTENER HOLE; STA 500D; STR. 19L; 6' OUTBOARD OF FUSELAGE SKIN<[01] REMOVED L/H WING L/E ATTACH ANGLE STA 500D STR 19L;6 OUTBOARD OF FUSELAGE SKIN I/A/W SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED ALL FASTENERS INTO NEW L/E ATTACH ANGLE IAW SRM 51-40-05-0G-0;[03] POLY GRAY PAINTED NEW L/E ANGLE IAW AMM 51-21-73-370-801;[04] VERIFIED STEP 2<BR>AND 3;[05] INSTALLED NEW L/E ATTACH ANGLE IAW SRM 51-40-02-0G-0;[06] VERIFIED STEP 5;[07] AUDIT CW