As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ABORTED TAKEOFF AT 90 KTS ACCOUNT NR 1 ENG PROBLEM. *S/D* ENG FAILURE LIGHT ON. FOUND NR 1 ENGINE HI-STAGE BLEED VALVE CLAMP BLOWN OFF AT DUCT TO HIGH STAGE VALVE INTERFACE. EXTENSIVE DAMAGE TO SURROUNDING AREA REVERSER BLANKETS. ATTACH CLAMP WAS INSTALLED INCORRECTLY DUE TO ALIGNMENT FINGER INTERFERENCE. MAINTENANCE ERROR BY GE ON-WING SUPPORT. CORRECTLY INSTALLED CLAMP AND REPAIRED ALL RESULTANT DAMAGE.