As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON THE NR 1 ENGINE INLET LIP SKIN EXTERNAL SURFACE. THERE ARE THREE FASTENERS ABOVE THE OTBD SEAM THAT ARE PULLING THROUGH. REMOVED LOOSE FASTENERS IAW SRM 51-40-02. REAMED FASTENER HOLES TO FIRST OVERSIZE IAW SRM 54-10-01-1A-2 TABLE 101. PERFORMED FASTENER HOLE PROBE INSPECTION IAW NDT PART 6-51-00-00 PROCEDURE 16. NO DEFECTS NOTED. INSTALLED NEW FASTENERS IAW SRM 54-10-01-1A-2 AND SRM 51-40-02.