What was found
(CAN) DURING AN MPI OF THE GEAR BELLCRANK A FATIGUE CRACK WAS DISCOVERED ON THE TOE OF THE FILLET WELD APPROXIMATELY 1/8 INCH IN LENGTH. PART WAS REJECTED, SEE ATTACHMENTS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
(CAN) DURING AN MPI OF THE GEAR BELLCRANK A FATIGUE CRACK WAS DISCOVERED ON THE TOE OF THE FILLET WELD APPROXIMATELY 1/8 INCH IN LENGTH. PART WAS REJECTED, SEE ATTACHMENTS.