As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE CLIMBING THROUGH 14000 FT LEFT ENGINE EXPERIENCED A COMPRESSOR STALL. ENGINE SELF RECOVERED AND CLIMB CONTINUED TO FL260. EGT REDLINED, THROTTLE RETARDED TO IDLE. ENGINE WAS REMOVED FOR METAL IN THE TAILPIPE, IT HAD A NORMAL ECM TREND PLOT. AT ENGINE TEARDOWN, A STAGE 2 TURBINE BLADE FAILURE WAS FOUND TO BE THE CAUSE.