As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H WING LEADING EDGE SKIN; 1EA FASTENER HOLE; #10 FROM OUTBOARD; ZONE 2 FASTENER ROW (IAW 57-41-01-2R-7 FIG. 202); HAS CRACK INDICATION FROM HFEC INSPECTION. / [01] FASTENER HOLE IS AT MAXIMUM OVERSIZE; .263' DIA.; IAW 57-41-01-2R-7.;[02] REPAIRED IAW EA 22-157-02024;[03] REPAIRED IAW EA 22-157-02024 C/W INSPECTION;[04] REPAIRED IAW EA 22-157-02024 C/W INSPECTION