As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHEN NR 2 ENGINE POWER ADVANCED TO 1.2 EPR AND STABLE FOR A CROSSBLEED START, THE NR 2 ENGINE COMPRESSOR STALLED. EGT WAS RISING THROUGH 680 CELSIUS WHEN THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED ENGINE PER MM 71-00-00 FOR STALL WITH NO DEFECTS NOTED. BORESCOPE REVEALED NO DEFECTS. EXACT PART CAUSING PROBLEM TO BE DETERMINED.