What was found
CORROSION ON INTERNAL STRUCTURE TO ATTACH CLEVIS IN XV2=325 ON OTBD VANE OF OTBD FLAP AT LT WING. OTBD VANE OF OTBD FLAP AT LT WING WAS REPLACED IAW SRM 57-50-14, FIG 2 SH 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON INTERNAL STRUCTURE TO ATTACH CLEVIS IN XV2=325 ON OTBD VANE OF OTBD FLAP AT LT WING. OTBD VANE OF OTBD FLAP AT LT WING WAS REPLACED IAW SRM 57-50-14, FIG 2 SH 2.