As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING -C- CHECK, NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME CRACKED IN FWD LOWER RADIUS. REMOVED AND REPLACED AT NR 2 SLAT AT ACT ROD END ATTACH HAS INBOARD ATTACH FRAME BY FWD LOWER 2 EA RIB SUPPORT PO 413627 P/N 65-17310-4 AND PIL 413644 P/N 65-17310-3 IAW B727 SRM 51-30-2. ACCOMPLISHED SLATS OPS CHECK, FOUND OK IAW B727 MM 27-81-0.