What was found
(CAN) DURING INSTALLATION, A REAR INBD ENGINE MOUNT, 1 OF THE 4 ANCHOR NUT BROKE AFTER THE REQUIRED TORQUE WAS REACHED IAW AMM CHAPTER 71-20-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING INSTALLATION, A REAR INBD ENGINE MOUNT, 1 OF THE 4 ANCHOR NUT BROKE AFTER THE REQUIRED TORQUE WAS REACHED IAW AMM CHAPTER 71-20-00.