This specification defines the requirements for externallythreaded fasteners manufactured from three different material typesidentified in Table I: 125 ksi UTS min for alloy steel (Type 1) andcorrosion resistant steel (Type 2), and 62 ksi UTS min for aluminum(Type 3).
Receiving contractors may reject any manufactured lot which doesnot conform.
Workmanship of fasteners shall conform with aircraftmanufacturing processes.
Recommendations for improvements or corrections to thisspecification should be directed to the Executive Secretary of theNational Aerospace Standards Committee or a using membercompany.
Specifications listed herein, of the issue in effect on date ofinquiry are a part of this specification to the extent indicated.In the case of conflict, the requirements herein shall takeprecedence.
- Edition:
- 3
- Published:
- 06/29/2012
- Number of Pages:
- 11
- File Size:
- 1 file , 95 KB
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