As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ABORTED TAKEOFF DUE TO AUTOFEATHER WOULD NOT ARM. COMPLIED WITH FLIGHT CREW PROCEDURES. REMOVED AND RANG OUT THE NR 2 ENGINE STRUT HARNESS AND REINSTALLED . CHECKED GOOD IAW PDT -8 RUN MANUALS. R & R THE NR 1 ENGINE STRUT HARNESS IAW MM 72-01-10.