The formation and accretion of ice on aircraft wings during flight can be potentially disastrous and existing in-flight de-icing methods are either bulky or power consuming. This paper investigates the use of shear wave de-icing driven by a macro fibre piezoelectric composite actuator on a composite plate typically used for aircraft wings. While the few existing research on this novel de-icing approach focused on either theoretical studies or single frequency mode optimisation that required high excitation amplitudes, this study revealed that the use of multimodal excitation through broadband frequency sweeps has the potential to promote the chance of shear stress induced de-icing at a relatively small excitation amplitude. The results reported here form the foundation for a pathway towards low power and lightweight de-icing mechanism for in-flight aircraft wings.Index Terms-De-icing, shear wave, piezoelectric, carbon fibre reinforced plastic (CFRP), macro fibre composite (MFC)