Using composite materials in primary structures requires careful consideration of the ability of the material to withstand service loads, particularly the resistance to impact loads generated through contact with objects during flight or routine maintenance. While perhaps not causing immediate failure of the structure, even small, barely visible levels of damage can cause a decrease in stiffness or strength. It is important to detect this damage at an early stage, lest the damage grow and the strength of the structure be reduced to the level of service loading.