As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BGM- DURING ROUTINE MAINTENANCE VISIT WHILE PERFORMING TASK 2750/02, RIGHT OUTBOARD FLAP, INBOARD JACKSCREW STOP ASSEMBLY WAS FOUND CRACKED. CRACK VERIFIED USING EDDY CURRENT TESTING. ACTUATOR REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL 27-52-24. CYCLED FLAPS SEVERAL TIMES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.