What was found
DURING CLIMB, THE NR 2 ENGINE DID NOT ADVANCE TO FULL CLIMB THRUST FROM REDUCED THRUST FOR 45 SECONDS. R & R NR 2 ENGINE FUEL PUMP IAW AMM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CLIMB, THE NR 2 ENGINE DID NOT ADVANCE TO FULL CLIMB THRUST FROM REDUCED THRUST FOR 45 SECONDS. R & R NR 2 ENGINE FUEL PUMP IAW AMM.