As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE WOULD NOT ACHIEVE CLIMB POWER. THE THROTTLE WAS FIRE WALLED DURING CLIMB, ALL INDICATIONS CONSISTANTLY LESS THAN 1 & 3. REMOVED AND REPLACED THE NR 2 ENGINE FUEL PUMP IAW AMM 73-12-01-2. REMOVED AND REPLACED MEC IAW AMM 73-20-01-2. PREFORMED A MAX POWER RUN IAW JRH CHP. 07. ALL POWER SETTINGS NORMAL, NO LEAKS NOTED.