As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE, N1 ROLLED BACK 10% AT CLIMB OUT. REF TTG8Q01BFMVQ FOR REPLACEMENT OF HMU AND FUEL PUMP PACKAGE. PERFORMED TESTS 8; 12 AND 13 PER POWER PLANT TEST REFERENCE TABLE AMM 71-00-00. TESTS PASSED. PERFORMED TASK 71-00-00-SWA-823-F00, LEAK CHECK AFTER 85% N1 ENGINE RUN IAW AMM 71-00-00. VERIFIED TASK MT 773-11-00 WAS COMPLIED WITH PREVIOUSLY.