As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND CRACKS ON THE LOWER SIDE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL. THE CRACKS WERE CONFINED TO THE BONDED INTERNAL DOUBLER AT ONE FASTENER HOLE, 5.2 INCHES OB OF THE STA 188 RIB. THE AREA WAS REPAIRED IAW ECRA 5510-01695.