As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE R/H FWD SKATE ANGLE IS WORN AS MARKED / REMOVED DAMAGE AT RH FWD SKATE ANGLE IAW SRM 53-80-13-1A-1. ORIGINAL THICKNESS .063'; AFTER REWORK .050' .013' MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-13-1A-1 FIG 104. TOOL: 18173 DUE: 11/27/20 REMOVED OUT OF LIMITS SKATE ANGLE AND INSTALLED NEW SKATE ANGLE ALL IAW SRM 51-40-02-0G-0 AND DWG 147A0030 REV A. RESTORED FINISH IAW AMM 51-21-73-370-804. ATAG# SU1144