What was found
CRACK ON RIB FORMER STA X05=408 AT FIXED LEADING EDGE INTERNAL STRUCTURE, LT WING. RIB FORMER STA X05=408 AT FIXED LEADING EDGE INTERNAL STRUCTURE , LT WING WAS REPAIRED PER SRM 57-06B FIG 23, SRM 51-30-2, SRM 51-30-5.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON RIB FORMER STA X05=408 AT FIXED LEADING EDGE INTERNAL STRUCTURE, LT WING. RIB FORMER STA X05=408 AT FIXED LEADING EDGE INTERNAL STRUCTURE , LT WING WAS REPAIRED PER SRM 57-06B FIG 23, SRM 51-30-2, SRM 51-30-5.