What was found
DURING OVERHAUL INSPECTION MULTIPLE CRACK INDICATIONS WERE FOUND DURING ULTRASONIC INSPECTION (IAW SB 61-58 APPENDIX C, SCAN B) HUB S/N 110502 WAS DISASSEMBLED AND REMOVED FROM SERVICE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OVERHAUL INSPECTION MULTIPLE CRACK INDICATIONS WERE FOUND DURING ULTRASONIC INSPECTION (IAW SB 61-58 APPENDIX C, SCAN B) HUB S/N 110502 WAS DISASSEMBLED AND REMOVED FROM SERVICE.