As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RH HORIZONTAL STAB INBD SIDE OF RIB AT STAB STA. 92.70 IS CRACKED AT THE LOWER TRANSITION RADIUS OF THE NO 2 VERTICAL STIFFENER. CUT AND REMOVED THE DAMAGE FROM THE RIB AND WEB AS SHOWN IN FIGURE 202 REPAIR 4 IAW SRM 55-10-09-2R-4. FABRICATED REPAIR PARTS -1 T-SECTION, -2 ANGLE AND -3 SHIMS 2EA AND INSTALLED REPAIR PARTS IAW SRM 55-10-09-2R-4 REPAIR 4.