As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT ENGINE FAILED TO ATTAIN T/O N1 POWER. AFTER MULIPLE ATTEMTS AND AN A/C "RESET" THE BEST N1 ATTITUDE WAS 68%, N1 WITH 100% N2 INDICATED. ON FINAL ATTEMT A COMPRESSOR STALL OCCURRED. REPLACED COMPRESSOR BLEED VALVE. SERVO VALVE/TORQUE MOTOR. INSTALLED SECONDARY ORIFICE P/N 30J1296CL40 ACCOMPLISHED ENGINE POWER RUN IN AUTO AND MANUAL MODE PER AIRCRAFT FLIGHT MANUAL AND FOUND SATISFACTORY. ALL WORK DONE IAW ENGINE MM 72-00-00 AND 71-00-00 AND 75-30-01.