COTS sensors and components have been combined into small, robust sensor modules, which can be attached to an aircraft structure. Data is collected and processed onboard the module, then transferred to an external server; the user can display the data and interact with the modules using a bespoke Graphical User Interface (GUI). The Structural Health Monitoring methods include point source techniques: Resistance Strain Gauges (RSGs) and Fibre Bragg Gratings (FBGs); and full-field techniques: Digital Image Correlation (DIC) and Thermoelastic Stress Analysis (TSA). Data is processed in near real-time, and indications of damage initiation and growth are shown as strain and stress field changes during loading.