As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THRUST LOSS OCCURRED MULTIPLE TIMES WITH NR 2 ENGINE. REMOVED AND ROUTED THE EEC, PERFORMED A DATA DUMP, NO FAULTS OR FAILURES FOUND. THE EEC BEING MADE SERVICEABLY AND RETURNED. REMOVED THE N2 TRANSDUCER ALTENATOR STATOR. CONPONENT PASSED ALL ELECTRICAL TEST, CANNON PLUG CONNECTOR DIRTY, THREADS ON SCREW ON BODY. COMPONENT LIKELY CAUSE. NO ISSUE ON ENGINE SINCE REPLACEMENT.