As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A DELAMINATION OF THE RIGHT HORIZONTAL STAB UPPER SKIN PANEL, WAS DETECTED DURING A GENERAL VISUAL INSPECTION OF THE AREA. THE DEBOND IS OPP. 40 INCHES X 12 INCHES, 21 INCHES OUTBOARD OF THE ROOT AND CENTER FORWARD AND AFT. THERE IS NO SIGNIFICANT VISUAL DAMAGE OF THE AREA. PRESUED CAUSE IS FATIGUE AND OR CORROSION.