As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT EXT FUSE SKIN AT FILLET FRG PANEL INTERFACE IS FRETTED BS 720D 10 TO 720E, STR 19R TO 4" ABOVE STR 18R REMOVED LEADING EDGE FOR ACCESS TO REPAIR. INSTALLED EXTERNAL REPAIR AT LAP SPLICE REF SRM 53-30-3 PG 20. REINSTALLED LEADING EDGE AND LEAKED CHECKED HYD LINES. REF 27-81-000-2 AND LEAK CHECKED TAI DUCT REF WO NR 35039/WC NR 70C53-00.