As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING TAKEOFF RIGHT ENGINE DID NOT SPOOL UP. RIGHT THRUST LEVER WAS SUBSTANTIALLY FRAIL TO BE UNRESPONSIVE TO INPUTS. REMOVED AND REPLACED; RH ENG. T/R POSITION FEED BACK TRANSDUCER IAW AMM 78-36-03. RIG CONFIRMED. REQUIRES HIGH POWER RUN TO COMPLETE OPERATIONAL CHECK. ITEM 3:PERFORMED MAX POWER ASSURANCE TEST IAW 71-00-00. OPS CHECK OF T/R GOOD AT THIS TIME. ENGINE DOES NOT LAG. DATA-TEMP="1"