Structural Weldbonding of Aluminum Structures
- Aerospace Standard
- ARP1675
- Reaffirmed
Scope
Rationale
Recommended Content
Aerospace Standard | Surface Preparation and Priming of Aluminum Alloy Parts for High Durability Structural Adhesive Bonding |
Aerospace Standard | Bearings, Sleeve, Plain and Flanged, Self-Lubricating |
Aerospace Standard | Bearings, Sleeve, Plain and Flanged, Self – Lubricating -65 to +250 °F |
Topic
Data Sets - Support Documents
Title | Description | Download |
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Unnamed Dataset 1 | ||
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TABLE 1 | Adhesive Primer Requirements | |
TABLE 2 | Visible External imperfections of Welds | |
TABLE 3 | Mechanical Property Requirements for Spotweld Sheet Requirements | |
TABLE 4 | Nugget Diameter | |
Unnamed Dataset 9 | ||
Unnamed Dataset 10 | ||
TABLE 5 | Production Meld Process Control Specimens | |
Unnamed Dataset 12 | ||
Unnamed Dataset 13 | ||
Unnamed Dataset 14 | ||
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Unnamed Dataset 16 | ||
Unnamed Dataset 17 | ||
Unnamed Dataset 18 |
Issuing Committee
AMS P17 Polymer Matrix Composites Committee
AMS P-17, Polymer Matrix Composites, is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain material specifications and other SAE technical reports for composite materials, including prepregs, reinforcing fibers and fabrics, matrix resins, adhesives, and core materials. The committee works in conjunction with related bodies such as the Composite Materials Handbook -17 (CMH-17), ASTM Committee D30 on Composite Materials, the National Center for Advanced Materials Performance (NCAMP), the Performance Review Institute (PRI), and regulatory authorities such as FAA and EASA.