As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT ENGINE HAD 3 COMPRESSOR STALLS DURING CLIMB THROUGH 16,000 TO 17,000 FT. DURING TROUBLESHOOTING FOR COMPRESSOR STALL FOUND DAMAGED 1ST STAGE FAN BLADE. PERFORMED VISUAL INSP OF BLADE DAMAGE, BLADE BENT 1 ¼ (L/E TO T/E) AND 1 24/32 (TIP TO SHANK) WITH NO CRACKS OR TEARS FOUND. REPAIRED BEND BLADE IAW AMM 72-33 FIG 801. ADDITIONALLY PERFORMED BOROSCOPE OF LPC AND HPC AND COMBUSTION CHAMBERS PER AMM 71-00-00 & 72-00-00. NO DEFECTS NOTED.