As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE HAD A COMPRESSOR STALL/PARTIAL POWER FAILURE DURING FINAL APPROACH AND LANDING INTO DTW ENGINE POWER EXCEEDED THAT QA LIMIT BY APPROX .05 FOR IMMEDIATELY PRIOR TO STALL/POWER LOSS. REMOVED AND REPLACED NR 2 ENGINE IAW MM 71-00-00. (M)