Composite Structures Question
For starters - Happy 2024!
In the US FAA AMT (aircraft maintenance technician) general handbook (8083) - speaking about ultrasonic inspection, different types of laminate defects are discussed. Can anyone here fill me in what defect (closure member and core-to-closure member) is being mentioned here? Any information is greatly appreciated - in this case - Google is not my friend - coming up empty handed. Thanks very much!!!
Type IV—voids in foam adhesive or disbonds between the adhesive and a closure member at core-to-closure member joints