As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(A-204 DOT 02); RH WING L/E ATTACH ANGLE CRACKED AT FASTENER HOLE; STA 500D; STR. 19R; 6' OUTBOARD OF FUSELAGE SKIN.<[01] VERIFIED ITEM 1 OF STEPS 1 - 3;[02] OK TO APPLY TOP COAT;[03] APPLIED TOP COAT FINISH TO ATTACH ANGLE I.A.W MM 51-21-99-300-901;[04] VERIFIED ITEM 3;[05] JOB COMPLETE; AUDIT C/W