What was found
CRACKED ANGLE ON INTERNAL FIXED LEADING EDGE WS 228 AT RT WING. ANGLE AT INTERNAL FIXED LEADING EDGE WS 228 AT RT WING WAS REPLACED IAW SRM 51-40-02-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACKED ANGLE ON INTERNAL FIXED LEADING EDGE WS 228 AT RT WING. ANGLE AT INTERNAL FIXED LEADING EDGE WS 228 AT RT WING WAS REPLACED IAW SRM 51-40-02-0G-0.