And that should make aircraft uncontrollable?
In an aircraft with a fixed horizontal stabilizer traveling in excess of 400 knots, yes. The aircraft will fly to its "trimmed" condition which without the tab is going to be closer to 120-150 knots. This will result in stick forces requiring 200-225lbs per inch nose up as the aircraft hunts for the speed. Aircraft with movable horizontal stabilizers or simply with jammed trim controls will want to remain trimmed for the speed at which trim control was lost.
Because of this tremendous nose up pitch force, G forces in excess of 10G will be experienced (evidenced by the photographs showing the tailwheel extending due to the G force, which will occur around 9G in a Mustang) which will catch any airman off guard. Because their body isn't prepared for the instant onset of G forces, the blood immediately leaves their upper body and a blackout will ensue in about a second. Another factor to consider is even if you were somehow to retain consciousness the G Forces will be pushing you down and forward in the cockpit because the aircraft is also decelerating to get to the neutral trim speed roughly 300 knots below what it's currently flying at.
In other words, the trim tab in a Mustang goes at high speed, the pilot blacks out and you either have a fortunate recoverable situation such as Voodoo in the 1990s or you crash without ever knowing what happened, as likely happened in this case.