ASTM E2580-24 specifies the ultrasonic testing method for flat composite materials and sandwich core materials for aerospace applications, mainly including:
| Test Procedure | Applicable Scenarios | Frequency Range | Typical Defects |
|---|---|---|---|
| Procedure A (Pulse Echo) | Single-sided Contact/Non-contact Testing | 0.5-20MHz | Delamination, Debonding, Porosity |
| Procedure B (Through Transmission) | Double-sided automated testing | 0.5-20MHz | Core material debonding and foreign matter inclusion |
The standard requires that the test frequency be selected based on the acoustic properties of the material: low frequency (0.5-5MHz) is suitable for high-attenuation materials, and high frequency (5-20MHz) is used for thin plates or high-resolution testing.
A reference block containing the following artificial defects must be used:
When using single-probe working mode, special attention should be paid to the following:
Special requirements for dual-probe systems:
Main updates compared to the 2017 version:
Typical application scenarios include:
Inspectors must be certified to NAS410 or equivalent Level II and undergo practical review every three years.
| Verification Items | Period | Based on Standards |
|---|---|---|
| System Linearity | Annual | E1324 |
| Probe Performance | Semi-annual | E1065 |
| Mechanical Accuracy | Quarterly | E543 |
Must include: probe model/serial number, coupling agent type, scanning path diagram, reference block number, gain setting parameters, etc. 23 key data.

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