As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER SKIN AT FRONT SPAR PITCH LOAD FITTING AREA, 1 EA FASTENER HOLE FOUND CRACKED AT WING UPPER SKIN RUNNING INBD & OTBD DIRECTION REFER TO REPORT FOR DETAIL. C/A 1EA FASTENER CRACK HOLE REPAIR ACCOMPLISHED IAW WORKCARD 5724-01005-12 AND VA82327 ADMA REV C, ISSUE DATE 05/31/2013.