As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT MAIN GEAR STRUT DOOR HAS DAMAGE ON L/E AT MID POINT WITH SKIN MISSING AND OPEN TO CORE FOAM. OPEN AREA IS 4 BY 1-2 WITH L SHAPED CRACK 2 INCH BY 1 INCH AT LWR EDGE OF DAMAGE CONT OF AMIS ITEM 4482001. ACP INTERIM REPAIR PER EVA -73721, TAPE RECHECK REQUIRED PRIOR TO EACH DEPARTURE, PERMANENT REPAIR IN 150 HRS. ACCMP'D REPAIRED IAW SRM.