As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE SKIN PANEL IS SEVERELY NICKED AND GOUGED FROM BS 1010 TO 1090 STR 20 TO 26R, REQUIRING REPLACEMENT OF PANEL. SKIN IS OUT OF LIMITS PER FEDEX SRM. REMOVED DAMAGED SKIN AND REPLACED WITH NEW AT STA 1010 TO 1183 STR 20 TO 26R, IAW FEDEX SRM 51-30-2, BAC DRW 65-54583 AND EA NR 7-5300-25594.