As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ETOPS SIGNIFICANT SYS - ATB - RT ENG BLEED LIGHT ON AT TOP OF CLIMB. COMPLIED WITH TSI IAW FIM 36-10-00 FIG 111 AND WD 36-11-62, WIRING BETWEEN BLEED CONTROL CARD AND HPC CONNECTOR, CHECKED GOOD. LEAK CHECKED ALL SENSE LINES, NO LEAKS FOUND. R & R HPC IAW MM 36-11-08-404. PERFORMED HIGH POWER RUN AND OPS TEST BLEED AIR SYSTEM IAW 36-11-00-715, SYS TEST NORMAL. BLEED AIR INDICATION BETWEEN BOTH ENGINES 2 PSI SPLIT AT HP SCHEDULED.