Structural Health Monitoring (SHM) via Guided Ultrasonic Waves (GUW) has been the subject of research for years and has already been described in detail for purely isotropic and purely anisotropic materials. Fibre Metal Laminates (FML) combine isotropic metal layers with anisotropic fibre composite layers to a laminate. They are mainly used in the aerospace industry to reduce mass while optimizing stiffness and strength properties. On the other hand, the combination of different materials leads to high differences in the acoustic impedance at the interfaces, which in turn leads to the question to what extent these materials can be monitored via GUW. This research investigates the applicability of polyvinylidene fluoride (PVDF) foil sensors for the detection of GUW in the interior of an Aluminium Glass Fibre laminate. Preliminary analytic investigations based on new adaptions of the partial-wave method gave insight into general GUW characteristics along fibre-metal interfaces and within an FML plate waveguide. Analytic and transient finite element simulation results were used to predict displacement fields. Composition and dimension of fabricated FML plates as well as excitation frequency were chosen based on these predictions, particularly maximizing dominance of the in-plane displacement components. For manufacturing the FML specimen with embedded PVDF sensors, a cold-curing epoxy resin was used to prevent the temperature-sensitive sensors from being destroyed or depolarized during production. After the design and application of a PZT actuator on the laminate, GUW were excited with particular attention to the frequencies in which a particularly dominating in-plane displacement field was assumed. Laser-Doppler Vibrometry (LDV) was used for measurements of the GUW's out-of-plane component.