As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE THICKNESS OF THE GAP BETWEEN THE INNER CHORD AND STRINGER S-18A RECORDED GAP VALUE .021 (GAP MEASUREMENT IS GREATER THAN 0.006 INCH)<[01] SHIMED GAP PER 5311-E-14625-NG;[02] C/W INSPECTION;[03] C/W INSPECTION