Morphing wing technologies provide expanded functionality in piloted and robotic aircra, extending particular vehicle mission parameters as well as increasing the role of aviation in both military and civilian applications. However, realizing control surfaces that do not void the bene�ts of morphing wings presents challenges that can be addressed with micro�ber composite actuators (MFCs). We present two approaches for realizing control surfaces. In one approach, �ap-like structures are formed by bonding MFCs to each side of a metal substrate. In the other approach, MFCs are bonded directly to the wing. Counter intuitively, the �ap approach resulted in larger voltage actuation curvatures, with increased mass load. Actuation performance, de�ned as the ratio of curvature per applied voltage, was as large as 5.8 ± 0.2 × 10 −4 (kV⋅mm) −1 . e direct bonding approach reveals that at zero wing pressure, up to 63 ± 3 m of displacement could be realized.