Max speed of the P-51 D was 437 mph (703 km/h)
For those who are unfamiliar with what they do, trim tabs are used to cause the airflow to deflect the Primary Flight Control surface. So, an elevator trim tab is deflected up to cause the elevator to deflect downwards, pointing the nose of the aircraft down, in relation to the relative wind.
Contrary to popular belief, the elevator does not make the plane go up; it simply raises and lowers the nose wrt the relative wind.If the elevator is in neutral position (Airplane flying level) and more power is added, the airplane will climb. Down elevator is applied to keep the plane flying at a constant altitude, and the result is more speed
So the trim tab is exposed to loading by the airflow--the higher the speed, the more force on the tab and its hinges and actuator.
And airflow is not constant--there are variations, all the time--and if you get into a flutter situation (Load variation frequency=natural frequency), the thing can go from "here to completely gone" in literally no time at all...