As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT EXTERNAL FUSE SKIN IS FRETTED AT FILLET FAIRING PANEL INTERFACE AT BS 720D 10", STRINGER 19L. 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. MM 27-81-000-2 (HYD LEAK CK) AND T.A.I DUCT LEAK CHECK ACCOMPLISHED.