As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AS A RESULT OF ULTRASONIC INSPECTION ON HORIZONTAL STABILIZER CONTSTANT OUTBOARD SKIN PANELS FOUND A .75 INCH CRACK ON NR 3 PANEL EMANATING FROM BOLT HOLE NR 29 TO BOLT HOLE NR 30 RIGHT SIDE, REF TO DOUGLAS SB A55-16. REPAIRED PER S/B.