This study is concerned with reducing the tonal noise emitted by electric ducted fans which serve as the propulsion system for a variety of unmanned aerial vehicles (UAVs). The underlying concept is utilizing the shroud pressure fluctuation caused by the rotating blades to drive the over-the-rotor (OTR) acoustic treatment and generates a secondary sound field that cancels the primary ducted fan sound field. Experiment shows a considerable destructive effect can be made by meticulous tuning of the strength and phase of the secondary source. In view of the space constraints of a real electric ducted fan, the acoustic treatment is reconfigured as a labyrinth-type acoustic metamaterial that reduces the structure size while maintaining the noise reduction performance at the same time. An advantage of the proposed technique is that each tone can be dealt with by a specifically designed acoustic treatment occupying a small patch on the fan shroud. Hence, a compact multi-tonal noise control solution is possible by circumferentially deploying several OTR acoustic treatments.