I wonder if
@wanttaja has any data on how often this happens?
I've read ~4400 homebuilt accident reports, and another ~4000 for production-type aircraft, but don't recall any mention of static wicks. I did a quick search of the 2009-2018 database for all aircraft. Got four hits for "static wick"...
Narrative - 2009-2018
ERA11FA312
CEN12FA487
CEN13IA285
ERA16FA043
In ERA11FA312, it's just referencing the location of fuel leak in relation to a static wick location.
CEN12FA487 referred to "The static wicks on the ailerons, elevator, and rudder were tested using a MEG OHM tester. All static wicks were found to test between 6 to 15 MEG OHMS with 1,000 volts applied, which was within allowable limits."
CEN13IA285 was a Cirrus, and the report said, "There were no static wicks installed on the airplane." Interesting case, static caused by precipitation interfered with communications.
ERA16FA043, a Beech A36, they were just mentioned in passing: "According to a logbook entry dated November 13, 2015, two defective static wicks were replaced, loose headphone jacks at the pilot and co-pilot positions were tightened, and troubleshooting of the primary turbine inlet temperature gauge occurred. There was no other documented maintenance performed before the accident flight." Probable cause was the failure to maintain airspeed on approach.
Ron Wanttaja