Adhesive-bonded components and structures have become an important part of manufacturing in the aerospace industry. These components often rely on honeycomb composite structures for strong yet lightweight design. However, the quality of the bonds is very important to the overall integrity of the composite structures. Due to their wide range of laminate and core configurations, these materials pose inspection challenges, especially during inspection for damage in the core, for example, disbonds and crushed core. For improved probability of detection (POD) on honeycomb composite structures, a multiple frequency C-scan-based approach exploiting both amplitude and phase C-scans is proposed.