As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A/C P-F CONV AT AERO WEAR WAS FOUND ON UPPER PORTION OF THRUST FITTING. PROBABLY CAUSED BY CONTACT WITH NR 2 ENG PRE-COOLER. THE AMOUNT OF WEAR IS NOT COVERED BY SRM 54-00. REPAIR REQUIRES INSTALL OF TWO NESTED REPAIR ANGLES FROM 0.063 THICK 6AL-4V ANNEALED TITANIUM AS PER FEDEX EA NR 8-5412-47997.