As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING NR 3 PYLON UPPER SURFACE GAP PANEL HAS 2 EA COMPOSITE CRACKS. STA ILES 666.22 CRACK IS 24.0 INCHES LONG AND AT ILES 670.22 CRACK IS 12.0 INCHES LONG. PERMANENT REPAIR ACCOMPLISHED IAW SRM 51-40-09, FIG 18, SHEETS 2 AND 5, 250 DEGREE CURE IAW SRM 51-40-12. EO 4757A483.