Non-destructive Inspection of Composite Aileron during Fatigue Test

The operational safety and reliability of an airplane must be integral part its design. use suitable materials that pass material certification tests is very important for a new aircraft next testing specific samples, sub-components, components such as the aileron. paper deals with non-destructive evaluation composite primary structural fatigue in accordance damage tolerance philosophy considering impact presence. NDT methods visual, eddy current, ultrasonic included phased array technique, are used inspections. A schedule inspections was created, durability verified.