As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 COMPRESSOR STALL IN DESCENT. [SUP 4-17-07] CAUSE WAS CIT SENSOR NOT RESPONDING TO TEMPERATURE CHANGE. REPLACED CIT SENSOR AND MAIN ENGINE CONTROL UNIT. MEC BENCH TEST FOUND NO FAULTS. CIT SENSOR DID NOT RESPOND TO TEMPERATURE CHANGE. BOTH UNITS MADE SERVICEABLE.