As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION OF LEFT AND RIGHT TRAPEZOIDAL PANEL PER SERVICE BULLETIN 53-182 RIGHT TRAP PANEL CRACKED EXTENDING FROM LEADING EDGE OF PANEL TO SECOND FASTENER. EDDY CURRENT BOLT HOLE INSPECTION CONFIRMS CRACK IS ONLY FROM FIRST HOLE TO FRONT EDGE OF PANEL LENGTH 1 INCH ROUTED OUT CRACK PER S/B 53-100. (M)