As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H VERTICAL TAIL SKATE ANGLE CHAFFING ON I/B SIDE BETWEEN STA 1016 TO STA 1016 +2' / REMOVED DAMAGE ON L/H SKATE ANGLE I/B SIDE STA 1016 TO 1016+2' IAW SRM 51-10-02-0G-0 MESSURED MATERIAL LOSS TO BE .004' ORIGINAL (T) .075' REMAINING (T) .071 FOUND TO BE IN LIMITS IAW SRM 53-80-13-1A-1. RESTORED FINISHES TO AREA IAW AMM 51-21-73-370-804.