Originally posted by helosailor
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At 450KIAS, the nose down trim would be substantial. So that means the elevator is at a pretty extreme (relatively) down angle and the trim tab is keeping it in place. Now imagine losing the trim tab at that point. The elevator would violently go from down to at a minimum, aligned into the wind. This would make the aircraft pitch up violently. The instantaneous G would be enough to make a 70-year old G-loc IMO.
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