As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK AT LAST RIVET HOLE IN THE FIXED SECTION ON O/B SIDE OF RT HORIZONTAL STABILIZER ELEVATOR ACCESS TO ELEVATOR GEAR TAB MECHANISM 3616A. THE PUSH ROD AND CONDUIT WERE REMOVED TO GAIN ACCESS IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 55-01, FIGURE 2 AND 51-30-8, THE PUSH ROD AND CONDUIT WERE REINSTALLED IAW SRM 51-30-2.