As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT 3500 FEET IN CLIMB HEARD ONE COMPRESSOR STALL FROM THE LT ENGINE THEN ENGINE PARAMETERS ALL DECLINED. COMPLETED ENGINE SHUT DOWN PROCEDURE AND RETURNED TO SJC. FOUND TURBINE DAMAGE AND REPLACED THE ENGINE. FOUND ONE NINTH STAGE COMPRESSOR BLADE HAD FRACTURED IN DOVETAIL ROOT SECTION. TWO OTHER NINTH STAGE BLADES FRACTURED IN AIRFOIL SECTION AND ALSO HAD CRACK INDICATIONS IN ROOT SECTION.