As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C, ON REMOVAL OF BS 940 LT FITTING 2 FASTENER HOLES THROUGH S18A AND FUSELAGE SKIN FOUND TO HAVE BEEN OVERSIZED AND OUT OF ED (AFT UPPER AT TACH BOLTS OF 940). INVESTIGATED AND REPAIR CARRIED OUT IAW SMRO EO 99-30-001 UPS ENGINEERING FILE NR 727-53-2170.