As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
REPAIRED VERTICAL CRACK FROM HOLE C-DOWN TO EDGE OF CUT OUT OF LT REAR SPAR UPPER CHORD BY OVERSIZING HOLE, FABRICATING AND INSTALLING BUSHING IAW REO-L0152 REV IR DATED 11-21-07 FAA FORM 8100-9. THIS IS A TIME LIMITED REPAIR, REPEAT INSPECTION REQUIRED AT 4500 AIRCRAFT CYCLES.