As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PHX-OMA - ABORTED TAKEOFF, NR 1 ENGINE HAD COMPRESSOR STALL ONCE WHEN POWER ADVANCED ABOVE IDLE. REMOVED AND REPLACED NR 1 ENGINE PRESSURE RATIO BLEED CONTROL ASSEMBLY, IAW BMM 75-31-11. ALSO, LUBRICATED INTERNAL BLEEDS PER EB 72-006. RAN ENGINES AND OPERATES NORMALLY. (M)