As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE #2 WOULD NOT ACHIEVE T/O THRUST. #1 WAS 92.9 WHILE #2 WAS 85 +- 0.3 WITH #2 THRUST LEVER FULL FORWARD. BURNED FUEL TO BELOW 10.1; LANDED AT 127.8 WT. / [01] PERFORMED THE VISUAL INSPECTION OF THE IMPELLER ROTATION IAW AMM 73-11-01-200-801-F00. FOUND THAT THE IMPELLER WAS NOT MOVING; SUSPECT FUEL PUMP DEFECTIVE.;[02] CW INSP;[03] CW INSP;[04] REMOVED AND REPLACED #2 ENGINE FUEL PUMP ASSEMBLY IAW 73-11-11 OPS CHECK /LEAK CHECK GOOD