What was found
LT WING SKIN UPPER LOAD FITTING ULTRASOUND CRACK INDICATION AFT FASTENER INBD ROW. REMOVED FASTENER, REAMED HOLE IAW WC 5724-01005-10. . REPAIRED COMPLETE ON PRI 515424-14AD REV 0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING SKIN UPPER LOAD FITTING ULTRASOUND CRACK INDICATION AFT FASTENER INBD ROW. REMOVED FASTENER, REAMED HOLE IAW WC 5724-01005-10. . REPAIRED COMPLETE ON PRI 515424-14AD REV 0.