As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
((WGFY)) THERE IS GAP L=2.73 INCH. W=0.78 INCH .T=0.029 BETWEEN LT LOWER SURFACE AND UNDER WING FUSE PIN FITTING PYLON NR 1 WING STA 116.8. PERFORMED A DETAIL VISUAL INSPECTION OF THE REPAIR ZONE, C-CHECK PERFORMED REPEAT DVI INSPECTION OF THE SUBJECT AREA IAW SB 747-54A2182 R2. REQUIREMENT AT 1200 FLIGHT CYCLES INTERVAL NOT TO EXCEED 24 MONTHS.