As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-11 CHECK A 2 INCH CRACK WAS FOUND ON L/H HORIZONTAL STABILIZER LOWER SKIN AT FORWARD OF INBOARD BALANCE PANEL, APPROXIMATELY 1 1/2 INCHES FORWARD OF REAR SPAR. MAINTENANCE STOP DRILLED CRACK ON LT HORIZONTAL STABILIZER LOWER SKIN AT FORWARD OF INBOARD BALANCE PANEL; PERFORMED HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW AWA E.R. 03-5513-03062-TB2A.