What was found
ROTOR ASSEMBLY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT, Q-ROTOR = 6.77 GMIN2. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3,128.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
ROTOR ASSEMBLY FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT, Q-ROTOR = 6.77 GMIN2. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3,128.