As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND DAMAGE FINS INSIDE THE NR 2 ENGINE PRECOOLER ALLOWING BLEED AND FAN AIR TO MIX. REMOVED RH ENGINE PRECOOLER IAW AMM 36-11-15, ITEM 11 INSTALLED PRECOOLER IAW AMM 36-11-15 FROM STEP PROCEDURE F AND UP/TO F(13). ITEM M12 COMPLETED STEP F(19) TO FINISH INSTALL IAW AMM 36-11-15, LEAK CHECK IS GOOD AT THIS TIME.