As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H VERTICAL STAB SKATE ANGLE WORN AND ERODDED / EVALUATED L/H VERTICAL SKATE ANGLE STA 1016 TO STA 1130 FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .063' REMAINING THICKNESS .028' LOSS OF .035' I/A/W SRM 53-80-13-1A-1 REMOVED AND REPLACED SKATE ANGLE P/N A48A8310U3 I/A/W SRM 51-40-02-0G-0 AND BOEING DRAWING 148A8300 REV C