As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) IT WAS DETERMINED THIS WEAR WAS THE RESULT OF THE FLAP ROLLERS P/N C6CWM1072-29, ALLOWING TOO MUCH FORE AND AFT MOVEMENT WHEN FLAPS WERE FULLY EXTENDED. NEW FLAP RODS P/N C6CW1083-1 INSTALLED AND ROLLERS ADJUSTED ACCORDINGLY. THERE WAS AN MRO FINDING REPORT GENERATED AND GIVEN TO VIKING AIR LIMITED TECHNICAL SUPPORT GROUP FOR THEIR INVESTIGATION INTO THIS WEAR ISSUE.