What was found
LT WING FLAP TRACK OTBD WORN OUT LIMITS THICKNESS REDUCTION D=.021" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED THE PERMANENT REPAIR IAW EA E175-57-169.1, REV IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LT WING FLAP TRACK OTBD WORN OUT LIMITS THICKNESS REDUCTION D=.021" REF SRM 57-52-03, TABLE 101. ACCOMPLISHED THE PERMANENT REPAIR IAW EA E175-57-169.1, REV IR.