As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FAULT - CRACK - CLIP, INTERNAL AFTER OUTBOARD SIDE FRAME OF NO.1 PYLON AFTER FAIRING, NAC STA 376.20 (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 88. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 88. AND BOEING DWG NO. 313T2303 SH. 136 REV. -. JOB COMPLETED.