What was found
(CAN) THREADED END BROKEN OFF DURING ASSY. (ENGINE POWER OUTPUT ADAPTOR SHAFT) (TC NR 20060605007)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) THREADED END BROKEN OFF DURING ASSY. (ENGINE POWER OUTPUT ADAPTOR SHAFT) (TC NR 20060605007)