As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND IN LT FRONT SPAR OF HORIZONTAL STABILIZER JUST INBOARD OF LT ATTACH RIB. CRACK APPEARED TO STOP UNDER SIDE AT FUSELAGE CONTACT POINT 2 INCHES FROM FRONT SPAR. SUSPECT CAUSE WAS WEAR INTO STABILIZER SKIN FROM FUSELAGE SKIN EDGE CONTACT. FUSELAGE SKIN RELIEVED TO PREVENT CONTACT. SEE FIGURE 8, CESSNA IPC MODEL 150.