As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) WHILE COMPLETING AN ANNUAL INSPECTION OF THE ACFT AND INSPECTING THE FLAP SYSTEM GENERAL INSPECTION A CRACK WAS NOTED ON THE LT INBD FLAP DRIVE ARM IN THE WEB RADIUS. THE CRACK WAS CLEARLY VISIBLE WITHOUT THE NEED FOR NDT. THE DRIVE ARM WAS R & R WITH A NEW PART. THE RT INBD DRIVE ARM WAS VISUALLY INSPECTED WITH NO CRACKS NOTED.