What was found
SECONDARY DAMAGE DUE TO BEARING FAILURE. SHAFT GROOVED. CORE UNIT RETAINED IN PHX BY ASE ENGINEERING FOR FURTHER INVESTIGATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 728.3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SECONDARY DAMAGE DUE TO BEARING FAILURE. SHAFT GROOVED. CORE UNIT RETAINED IN PHX BY ASE ENGINEERING FOR FURTHER INVESTIGATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES: 728.3.