As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING UPPER LEADING EDGE PANEL AT NR 2 ENGINE PYLON DELAMINATED AT PREVIOUS REPAIR JUST I/B OF L/E GAP PANEL. REMOVED DAMAGE LEADING EDGE PANEL IAW B-747-200 SRM 51-30-02.SENT TO OUTSIDE SERVICE AIRCRAFT CONNECTION INC. REPAIRED PER SRM 51-40-08 PAGE 1, SRM 51-40-09 FIG 1, SRM 51-40-12 PAGE 1 THRU 38 FIG 6 SHEET 1, REV 105. OK TO INSTALL. LOCATED INSTALLED AND SEALED IAW B-747-200 SRM 51-30-02 AND 51-10-06.