What was found
CREW REPORTED DURING CLIMB POWER, NR 2 ENGINE VIBRATION INDICATION AT 3.0 UNITS, AT APPROXIMATELY 88 PERCENT N1. VIBRATION FELT IN AIRFRAME. VIBRATION LEVEL DID DECREASE WITH REDUCTION IN N1 SPEED. NR 2 ENGINE REPLACED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CREW REPORTED DURING CLIMB POWER, NR 2 ENGINE VIBRATION INDICATION AT 3.0 UNITS, AT APPROXIMATELY 88 PERCENT N1. VIBRATION FELT IN AIRFRAME. VIBRATION LEVEL DID DECREASE WITH REDUCTION IN N1 SPEED. NR 2 ENGINE REPLACED.