As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INTERNAL FUSELAGE CAC AREA AT STA 1156 TO 1158 BETWEEN LONGERONS 31 TO 28 LT SIDE EXISTING REPAIR. PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P2 CRITERIA FOUND INSTALLED BOLTS INSTEAD OF HI-LOCKS IAW SRM 53-30-00 FIG 7 VOL 1. INSTALLED FASTENERS IAW SRM 53-30-00 FIG 7 VOL 1. PERFORMED INSPECTION IAW FEDEX EA NR 8-5330-99374 PART 1.