High induced drag is associated with low angles of attack. This statement is:

Induced drag is primarily associated with the generation of lift. It is crucial to understand that induced drag increases as lift increases and is typically more significant at higher angles of attack, where the lift is maximized. At low angles of attack, the aircraft does not generate enough lift to produce significant induced drag. Thus, it follows that a scenario characterized by low angles of attack results in low levels of induced drag.

The relationship becomes clearer when considering the lift-to-drag ratio. As an aircraft maneuvers at low angles of attack, it experiences better efficiency and decreased induced drag because it requires less lift. Therefore, the statement in question is indeed false, as high induced drag does not correlate with low angles of attack.