This specification defines the requirements for externally threadedfasteners manufactured from three different material types identified inTABLE I:125 KSI UTS Min for alloy steel (TYPE 1) and corrosionresistant steel (TYPE 2), and 62 KSI UTS Min for aluminum (TYPE 3).Receiving contractors may reject any manufactured lot which does notconform.
Workmanship of fasteners shall conform with aircraft manufacturingprocesses.
Recommendations for improvements or corrections to this specificationshould be directed to the Executive Secretary of the National AerospaceStandards Committee or a using member company.
Specifications listed herein, of the issue in effect on date ofinquiring are a part of this specification to the extent indicated.Inthe case of conflict, the requirements herein shall take precedence.
- Edition:
- 1
- Published:
- 03/22/2000
- Number of Pages:
- 11
- File Size:
- 1 file , 840 KB
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